Bibliography for Aircraft Parameter Estimation · Bibliography for Aircraft Parameter Estimation ... Aerodynamic Characteristics of Fighter Configurations During Spin Entries ...

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NASA Technical Memorandum 86804

Bibliography for Aircraft Parameter Estimation

Kenneth W. Iliff and Richard E. Maine

OCTOBER 1986

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https://ntrs.nasa.gov/search.jsp?R=19870020065 2019-07-19T07:08:16+00:00Z

NASA Technical Memorandum 86804

Bibliography for Aircraft Parameter Estimation

Kenneth W. Iliff and Richard E. Maine Ames Research Center Dryden Flight Research Facility Edwards, California

NASA National Aeronautics ana Space Administration

Scientific and Technical Information Branch

1986

PREFACE

A b i b l i o g r a p h y i s a u s e f u l source Of p o t e n t i a l re fe rences f o r research i n any f i e l d o f s tudy. An e x t e n s i v e b i b l i o g r a p h y has no t been a v a i l a b l e i n t h e f i e l d o f a i r c r a f t parameter e s t i m a t i o n , and t h i s document i s t h e r e s u l t o f an e f f o r t t o fill t h i s vo id . The l i s t i s ex tens i ve , a l t hough n o t exhaust ive, and does c o n t a i n d e f i n i t i v e works r e l a t e d t o most a i r c r a f t parameter e s t i m a t i o n approaches. T h e o r e t i c a l s t u d i e s as w e l l as p r a c t i c a l a p p l i c a t i o n s a r e included. Many of t h e s e p u b l i c a t i o n s a r e p e r t i n e n t t o s u b j e c t s p e r i p h e r a l l y r e l a t e d t o parameter es t ima t ion , such as a i r c r a f t maneuver des ign o r i ns t rumen ta - t i o n c o n s i d e r a t i o n s .

T h i s b i b l i o g r a p h y was generated by s o l i c i t i n g u s e f u l r e f e r e n c e m a t e r i a l f rom l e a d i n g i n t e r n a t i o n a l

There i s no c l a i m t h a t t h e l i s t i s complete. parameter e s t i m a t i o n s p e c i a l i s t s ; t h e p r imary c r i t e r i o n f o r i n c l u d i n g any re fe rence was t h a t i t be con- s i d e r e d meaningfu l by some s p e c i a l i s t s .

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BIBLIOGRAPHY

Anon.: T o t a l I n - F l i g h t S imu la to r (TIFS) - P r e l i m i n a r y Design Report. Techn ica l Repor t AFFDL-TR-71-119, pp. 25-26, Aug. 1971.

Anon.: Parameter E s t i m a t i o n Techniques and A p p l i c a t i o n s i n A i r c r a f t F l i g h t Test ing. NASA TN D-7647, 1974.

Abbot, W.Y.; Bo i run , B.H.; H i l l , G.E.: and Tavares, E.J.: F l i g h t E v a l u a t i o n Pacer Systems Low-Range A i r speed System LORAS 1000, F i n a l Report. C a l i f o r n i a , May 1977.

Acton, Forman S.: Numerical Methods t h a t Work. Harper & Row, New York. 1970.

AGARD: AGARD F l i g h t Test I n s t r u m e n t a t i o n Ser ies , vo l s . 1-15. AGARD-AG-160, 1972-1983.

AGARD:

US AAEFA P r o j e c t No. 75-17-1, Edwards A i r Fo rce Base,

Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n . AGARD-CP-172, May 1975.

AGARD: The E f f e c t s of B u f f e t i n g and Other Transonic Phenomena on Maneuvering Combat A i r c r a f t . AGARO-AR-82, J u l y 1975.

AGARD: S t a l l / S p i n Problems o f M i l i t a r y A i r c r a f t . AGARD-CP-199, June 1976.

AGARD: F l i g h t / G r o u n d T e s t i n g F a c i l i t i e s C o r r e l a t i o n . AGARD-CP-187, 1976.

AGARD: F l i g h t Test Techniques - of A i r c r a f t and Weapon Systems C o n t r o l . AGARD-CP-223, 1977.

AGARD: Dynamic S t a b i l i t y Parameters. AGARD-CP-235, 1978.

AGARD: High Angle of A t tack Aerodynamics. AGARD-CP-247, Jan. 1979 (a) .

AGARD: Parameter I d e n t i f i c a t i o n . AGARD-LS-104, 1979 (b) .

AGARD: Aerodynamic C h a r a c t e r i s t i c s o f Contro ls . AGARD-CP-262, May 1979 (c) .

AGARD: Dynamic S t a b i l i t y Parameters. AGARD-LS-114, 1981.

AGARD: Ground /F l i gh t Test Techniques and C o r r e l a t i o n . AGARD-CP-339, 1983.

A'Harrah, R.C.; Lamanna, W.J.; and Hodgkinson, J.: Are Today's S p e c i f i c a t i o n s A p p r o p r i a t e f o r Tomorrow's

Akaike, H i r o t u g u : A New Look a t S t a t i s t i c a l Model I d e n t i f i c a t i o n . I E E E Trans. Automat. C o n t r o l ,

Aeroplanes? S t a b i l i t y and C o n t r o l , AGARD-CP-260, Paper 23. May 1979.

v o l . AC-19, no. 6, pp. 716-723, Dec. 1974.

Angl i n , E.: Aerodynamic C h a r a c t e r i s t i c s o f F i g h t e r C o n f i g u r a t i o n s D u r i n g Spin E n t r i e s and Developed Spins. J. A i r c r a f t , vo l . 15, no. 11, pp. 769-776, Nov. 1978.

New York, 1967. Aoki , Masanao: O p t i m i z a t i o n o f S tochas t i c Systems; Topics i n D isc re te -T ime Systems. Academic Press,

Aoki , Masanao; and S t a l e y , R.M.: On Input S igna l Syn thes i s i n Parameter I d e n t i f i c a t i o n . P r e p r i n t s F o u r t h I n t e r n a t i o n a l F e d e r a t i o n o f Automatic C o n t r o l Congress, Warsaw, Poland, 1969.

Apos to l , Tom M.: Ca lcu lus : Volume 11. Second ed. Xerox C o l l e g e P u b l i s h i n g , Waltham, Massachussetts, 1969.

Ash, Rober t B.: B a s i c P r o b a b i l i t y Theory. John Wi ley & Sons, New York, 1970.

Astrom, K a r l J.: I n t r o d u c t i o n t o S tochas t i c C o n t r o l Theory. Academic Press, New

Astrom, K.J.; and Eykho f f , P.: System I d e n t i f i c a t i o n - a Survey. Automat ica, vo pp. 123-162, Mar. 1970.

York, 1970.

. 7, no. 2,

A t t l f e l l n e r , S.; and Rade, M.: 80 105 I n - F l i g h t S i m u l a t o r f o r F l i g h t C o n t r o l and Guidance Systems. F i r s t European R o t o r c r a f t and Powered L i f t A i r c r a f t Forum, Southhampton, Great B r i t a i n , Sept. 1975.

Bach, R.E.; and Wingrove, R.C.:

Ba lak r i shnan . A.V.: Communication Theory. McGraw-Hil l Book Co., New York, 1968.

Ba lak r i shnan , A.V.:

A p p l i c a t i o n s o f S t a t e E s t i m a t i o n i n A i r c r a f t F l i g h t Data A n a l y s i s . A I A A Paper 83-2087, Aug. 1983.

I n t r o d u c t i o n t o Op t im iza t i on Theory i n a H i l b e r t Space. Sp r inge r -Ver lag . B e r l i n , 1971.

n L

Ba lak r i shnan , A.V.: S tochas t i c D i f f e r e n t i a l Systems I. F i l t e r i n g and C o n t r o l ; A F u n c t i o n Space Approach. Notes i n Economics and Mathematical Systems, vo l . 84.)

M. Becklnann, G. Goos. and H.P. Kunzi, eds., Sp r inge r -Ver lag . B e r l i n , 1973. ( L e c t u r e

Ba lak r i shnan , A.V.: S tochas t i c F i l t e r i n g and Con t ro l . o p t i m i z a t i o n Sof tware, Inc., Los A n g e l s , 1981.

Ba lak r i shnan , A.V.: Kalman F i l t e r i n g Theory. O p t i m i z a t i o n Sof tware, Inc., New York, 1984.

Ba lak r i shnan , A.V.; and Peterka, V.: I d e n t i f i c a t i o n i n Automat ic C o n t r o l System, Automatica, v o l . 5, pp. 817-829, NOV. 1969.

Baner jee, D.; and Hohenemser, K.H.: A p p l i c a t i o n t o L i f t i n g Rotors.

Optimum Data U t i l i z a t i o n f o r Parameter I d e n t i f i c a t i o n w i t h J. A i r c r a f t , v o l . 13, pp. 1014-1016, Dec. 1976.

Comparison o f Gradient Methods f o r t h e S o l u t i o n o f Non l i nea r Parameter E s t i m a t i o n Bard, Yonathon: Problems. S I A M J. Numer. Anal ., vo l . 7, no. 1, pp. 157-186, Mar. 1970.

Barnard, G.A.: Thomas Bayes - A B i o g r a p h i c a l Note. B iomet r i ka , v o l . 45, pp. 293-295, 1958.

Ba t te rson , James G.: Analys is o f O s c i l l a t o r y Mot ion o f a L i g h t A i r p l a n e a t High Values o f L i f t C o e f f i c i e n t . NASA TM-84563, 1983.

t h e Ob jec t i ons o f t h e Author o f "The Analyst . John Noon, London, 1736. (Fo r a d d i t i o n a l i n f o r m a t i o n see Barnard, 1958.)

Bayes, Thomas: An I n t r o d u c t i o n t o t h e Doc t r i ne , ,o f F l u x i o n s , and a Defence o f t h e Mathemat ic ians Aga ins t

Bendix Corp.: A C I P E r r o r C o r r e c t i o n Models F i n a l Report. BSR 4426, C o n t r a c t NAS9-15588, Bendix Corpo ra t i on , Ann Arbor, Mich igan, kt. 1980.

Bennet t , G.E.: Mace, W.D.; and Pool, A.: Magnetic Record ing o f F l i g h t Test Data. F l i g h t Test I n s t r u m e n t a t i o n Ser ies , AGARD-AG-160, v o l . 5. Feb. 1974.

Benne t t , Robert M.; Farmer, Moses G.; Mohr, Richard L.: and H a l l , W. E a r l , Jr.: A Wind-Tunnel Technique f o r De te rm in ing S t a b i l i t y D e r i v a t i v e s from Cable-Mounted Models. J. A i r c r a f t , v o l . 15, no. 5, pp. 304-310, May 1978.

Aerospace Labora to ry , NLR TR 83091 U, The Nether lands, 1983.

1977. (Mathematics i n Science and Engineer ing, vo l . 128.)

Best , M.R.: Three-Dimensional F l i g h t - P a t h Recons t ruc t i on by Means o f S p l i n e Approx imat ion. Na t iona l

Bierman, Gera ld J.: F a c t o r i z a t i o n Methods f o r D i s c r e t e Sequent ia l Es t ima t ion . Academic Press, New York,

Box, George E.P.; and MacGregor, John F.: The A n a l y s i s o f Closed-Loop Dynamic-Stochast ic Systems. Technometrics, vo l . 16, no. 3, pp. 391-398. Aug. 1974.

Box, G.E.P.; and MacGregor, J.F.: Parameter E s t i m a t i o n w i t h Closed-Looped Opera t i ng Data. Proc. S i x t h I n t e r n a t i o n a l Federat ion o f Automatic Con t ro l , T r i e n n i a l World Congress, Boston and Cambridge, Massachussetts, 1975, Paper 38-5, 1975.

Bramwell, A. R. S.: H e l i c o p t e r Dynamics. Edward A rno ld Pub l i she rs , London, 1976.

Brauer , Fred; and Nohel, John A.: O u a l i t a t i v e Theory o f Ord ina ry D i f f e r e n t i a l Equat ions; an I n t r o d u c t i o n . W.A. Benjamin, New York, 1969.

Hawker Hunter Mk 7. Nat ional Aerospace Labora to ry NLR TR 83042, The Nether lands, 1983. Breeman: J.H.: Parameter I d e n t i f i c a t i o n R e s u l t s o f Tests i n Non-Steady Symmetric F l i g h t w i t h t h e

Breeman, J.H.; and Simons, J.L.: E v a l u a t i o n o f a Method t o E x t r a c t Performance Data f rom Dynamic Maneuvers f o r a Jet Transpor t A i r c r a f t . Proc. E leven th Congress o f t h e I n t e r n a t i o n a l Counc i l o f t h e Aeronau t i ca l Sc iences, Lisbon, Sept. 1978. v o l . 1, pp. 475-488, I n t e r n a t i o n a l Counci l o f t h e Aeronau t i ca l Sc iences S e c r e t a r i a t (DGLR), Cologne, 1978.

Breeman, J.H; E rke lens , L.J.J.; and Nieuwpoort, A.M.H.: De te rm ina t ion o f Performance and S t a b i l i t y C h a r a c t e r i s t i c s f rom Dynamic Manoeuvers w i t h a T ranspor t A i r c r a f t Using Parameter I d e n t i f i c a t i o n Techniques. N a t i o n a l Aerospace Labora to ry NLR MP 84024, The Nether lands, 1984.

I n s t r u m e n t a t i o n . Parameter I d e n t i f i c a t i o n , AGARD-LS-104, Paper 4, Oct. 1979. Breeman, J.H.: Van Woerkom, K.; Jonkers, H.L.; and Mulder, J.A.: Aspects o f F l i g h t Test

Brenner, M a r t i n J.; I l i f f , Kenneth W.; and Whitman, Rober t K.: E f f e c t o f Sampling Rate and Record Length on t h e Determinat ion o f S t a b i l i t y and Con t ro l D e r i v a t i v e s . NASA TM-72858, 1978.

B r i c z i n s k i , S.J., and Cooper, D.E.: F l i g h t I n v e s t i g a t i o n o f R o t o r / V e h i c l e S t a t e Feedback. NASA

B r o c k e t t , Roger W.: F i n i t e Dimensional L i n e a r Systems. John Wi ley 8 Sons, New York, 1970.

CR-132546, 1975.

3

I

B ryan t , W.H.; and Hodge, W.F.: A Monte Car lo Ana lys i s of t h e E f fec ts o f I n s t r u m e n t a t i o n E r r o r s on A i r c r a f t Parameter I d e n t i f i c a t i o n . AGARD-CP-172, Paper 5, May 1975.

Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n ,

Rryson, A r t h u r E., Jr.; and Ho, Y. Ch.: Appl ied Optimal C o n t r o l , Op t im iza t i on , E s t i m a t i o n and

Bucy, R icha rd S.; and Joseph, Peter D.:

C o n t r o l . Ginn and Company, Lex ington, Massachusetts, 1969.

F i l t e r i n g f o r S t o c h a s t i c Processes w i t h A p p l i c a t i o n s t o Guidance. I n t e r s c i e n c e Pub l i she rs , New York, 1968.

Bu r ton , R.A.: Advancement i n Parameter I d e n t i f i c a t i o n and A i r c r a f t F l i g h t Tes t i ng .

Caines. Pe te r E.; and Chan, C.W.: Feedback Between S t a t i o n a r y S tochas t i c Processes. I E E E Trans.

Caines, P.E.; and Sinha, S.:

Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 15, May 1975.

Automat. C o n t r o l , v o l . AC-20, pp. 498-508, Aug. 1975.

I d e n t i f i c a t i o n . Adap t i ve Processes, Houston, pp. 584-589, Dec. 1975.

An A p p l i c a t i o n o f t h e S t a t i s t i c a l Theory o f Feedback t o Power System Proc. 1975 IEEE Conference on D e c i s i o n and C o n t r o l , I n c l u d i n g t h e 1 4 t h Symposium on

Cannaday, R.L.; and S u i t : W.T.: E f f e c t s of Con t ro l I n p u t s on t h e E s t i m a t i o n o f S t a b i l i t y and Con t ro l Parameters o f a L i g h t A i rp lane . NASA TP-1043, 1977.

A i r Data Symposium, Naval Postgraduate School, Monterey, June 1976: Proceedings, Session V : Hel icoptor/VSTOL Sensors, Monterey, C a l i f o r n i a , 1976.

C o n t r o l . AGARD-AR-134, Jan. 1979.

C a r t e r , J.: The Measurement o f H e l i c o p t e r A i r Data Using a S w i v e l l i n g P i t o t - s t a t i c Pressure Probe.

Chalk, C.R.: Technica l E v a l u a t i o n Report on t h e F l i g h t Mechanics Panel Symposium on S t a b i l i t y and

Charon, W.; and Verbrugger, R.A.: Nouvelle Technique d ' e s s a i s sur Maquettes L i b r e s Pour l a De te rm ina t ion de C a r a c t E r i s t i q u e s A6rodynamiques; Paper 2, 1978.

Dynamic S t a b i l i t y Parameters, AGARD-CP-235,

Chen, R.T.N.: I n p u t Design f o r A i r c r a f t Parameter I d e n t i f i c a t i o n : Using Time-Optimal C o n t r o l Formulat ion. Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 13, May 1975.

Chen, R.T.N.; E u l r i c h , B.J.; and Lebecqz, J.V.: Development o f Advanced Techniques f o r t h e I d e n t i f i c a t i o n o f V/STOL A i r c r a f t S t a b i l i t y and Con t ro l Parameters. Cornel1 Aeronau t i ca l Lab., Inc., Rept. No. CAL-BM-2820-F-1, AD-730121, 1971.

C l a r k , Dan ie l C.; and D r o l l , John: General Purpose A i r b o r n e Simulator -Conceptual Design Report. NASA CR-544, 1966.

Corb in, M.: A P r e l i m i n a r y Study o f an Adapt ive F l i g h t Con t ro l System Using I n - F l i g h t I d e n t i f i c a t i o n

Cox, A.B.; and Bryson, A.E., Jr.: I d e n t i f i c a t i o n by a Combined Smoothing Non l i nea r Programming

Crambr. Harald. Mathemat ica l Methods o f S t a t i s t i c s . P r i n c e t o n U n i v e r s i t y Press, P r ince ton . New Jersey,

o f Three A i r c r a f t C o e f f i c i e n t s . RAE TR 75012, Mar. 1975.

A lgo r i t hm. Automat ica. v o l . 16, no. 6, pp. 689-694, Nov. 1980.

1946.

Davidon, W.C.: V a r i a b l e M e t r i c Methods f o r M in im iza t i on . A.E.C. Research and Development Repor t

Defalque, B.; Gevers, M.; and I n s t a l l e , M.: Combined I d e n t i f i c a t i o n o f t h e Input-Output and Noise

ANL-5990, Rev. Argonne Na t iona l Lab., Argonne, I l l i n o i s , 1959.

Dynamics o f a Closed-Loop C o n t r o l l e d L inear System. I n t . J. Con t ro l , vo l . 24, no. 3, pp. 345-360, Sept. 1976.

Numerical Ana lys i s , York, 1976, D. Jacobs, ed., The S t a t e o f t h e A r t o f k m e r i c a l A n a l y s i s , pp. 269-312. Academic Press, New York, 1977.

De Leo, R.V.; and Jensen, D.P.: Low Range Orthogonal A i r speed System. A i r Data Symposium, Naval Postgraduate School, Monterey, June 1976; Proceedings, Sess ion V: Hel icopter/VSTOL Sensors, Monterey, C a l i f o r n i a , 1976.

Dennis, J.E., Jr.: Non-Linear Least-Squares and Equat ions. Conference on t h e S t a t e o f t h e A r t i n

Derbyshi re , Thomas; and S idwe l l , Kenneth W.: PAN A i r Summary Document (Ve rs ion 1.0). NASA CR-3250, 1982.

Determann. 0.: E r m i t t l u n g von dynamischen D e r i v a t i v e n de r La'ngs-und Seitenbewegung m i t d e r mob i l en o s z i l l i e r e n d e n Der ivat ivwaage und systemat ische Untersuchungen zum E i n f l u s s e i n i n g e r Parameter auf d i e E rgeb in i sse . DGLR-78-115, Jahrestagung d e r DGLR, Darmstadt, 19-23 Sept. 1978.

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Deutsch, R.: E s t i m a t i o n Theory. P r e n t i c e H a l l , Englewoods C l i f f s , New Jersey, 1965.

Dixon, L.C.W.: Non l i nea r Op t im iza t i on . Crane, Russak & Co., New York, 1972.

Doetsch, K a r l H.: The Time Vector Method f o r S t a b i l i t y I n v e s t i g a t i o n s . A.R.C. R. & M. 2945, Aug. 1953.

Dongarra, J.J.; Moler , C.B.; Bunch, J.R.; and S tewar t , G.W.: I n d u s t r i a l and App l i ed Mathematics, P h i l a d e l p h i a , 1979.

DuBro, G.A.; K im, D.G.: and Rudd, M.J.: An E l e c t r o - o p t i c A i r speed Sensor. A i r Data Symposium, Naval Postgraduate School, Monterey, June 1976: Proceedings, Sess ion I V : Hel icopter/VSTOL Sensors, Monterey, C a l i f o r n i a , 1976. ( A l s o p u b l i s h e d i n E l e c t r o - o p t i c a l Systems Design Conference and I n t e r n a t i o n a l Laser Expos i t i on , New York, Sept. 14-16, 1976; Proc. Technica l Program, pp. 384-392, Chicago, 1976.)

LINPACK Users ’ Guide. S o c i e t y f o r

Edwards, John W.; Deets, Dwain A.: Development o f a Remote D i g i t a l Augmentation System and A p p l i c a t i o n t o a Remotely P i l o t e d Research Vehic le . NASA TN D-7941, 1975.

E r i csson , L.E.: Technica l E v a l u a t i o n Repor t on t h e F l u i d Dynamics Panel Symposium on Dynamic S t a b i l i t y Parameters. AGARD-AR-137, Apr. 1979.

E r i csson , L.E.: Support I n te r fe rence . Dynamic S t a b i l i t y Parameters, AGARD-LS-114, Paper 8, May

E t k i n , Bernard: Dynamics o f F l i g h t . John Wi ley & Sons, New York, 1959.

E u l r i c h , B.J.; and Rynaski, E.G.: I d e n t i f i c a t i o n o f Non l i nea r Aerodynamic S t a b i l i t y and C o n t r o l Parameters a t High Angle o f A t tack . Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n ,

1981.

AGARD-CP-172, pp. 2-1 t o 2-15, 1975.

E u l r i c h , B.J.; Gov inda ra j , K.S.; and Har r i ng ton , W.W.: E s t i m a t i o n o f t h e Aerodynamic S t a b i l i t y and C o n t r o l Parameters f o r the F-106A A i r c r a f t f rom F l i g h t Data: Maneuver Design and F l i g h t Data Ana lys i s . A I A A Paper 78-1326, 1978.

Eykho f f , P i e t e r : System I d e n t i f i c a t i o n , Parameter and S t a t e Es t ima t ion . John Wi ley & Sons, London,

Fagin, S.L.: Recurs i ve L inea r Regress ion Theory, Opt imal F i l t e r Theory and E r r o r A n a l y s i s o f Opt imal

Fe ik , R.A.:

1974.

Systems. I E E E I n t e r n a t i o n a l Convention Record, P a r t I, Session 30, pp. 216-240, 1964.

Department o f Defence Aerodynamics Repor t 161, Defence Science and Technology Organ isa t i on , Ae ronau t i ca l Research L a b o r i t o r i e s , Melbourne, V i c t o r i a , A u s t r a l i a , 1984.

On t h e A p p l i c a t i o n o f C o m p a t i b i l i t y Checking Techniques t o Dynamic F l i g h t Test Data.

Ferguson, Thomas S. : Mathematical S t a t i s t i c s : A D e c i s i o n T h e o r e t i c Approach. Academic Press, New York, 1967.

F i n d l a y , J.T.:

F ink , Marv in P.; and Freeman, Delma C., Jr.: F u l l - s c a l e Wind-Tunnel I n v e s t i g a t i o n o f S t a t i c

A C I P Performance Assessment D u r i n g STS-1 Re-Entry - Comparisons w i t h I M U Measurements and T r a j e c t o r y P r e d i c t i o n Considerat ions. AMA Rep. No. 81-26, Con t rac t NAS1-16087, Sept. 1981.

L o n g i t u d i n a l and L a t e r a l C h a r a c t e r i s t i c s o f a L i g h t Twin-Engine A i rp lane . NASA TN D-4983, 1969.

F i s h e r , R.A.: On t h e Mathematical Foundat ions o f T h e o r e t i c a l S t a t i s t i c s . Ph i l os . Trans. Roy. SOC. London, vo l . 222, pp. 309-368, 1922.

F i s h e r , Ronald A.: C o n t r i b u t i o n s t o Mathemat ica l S t a t i s t i c s . John Wi ley 8 Sons, New York, 1950.

F i ske , P.H.; and P r i c e , C.F.: A New Approach t o Model S t r u c t u r e I d e n t i f i c a t i o n . A I A A Paper 77-1171,

F l a c k , Nelson D.: AFFTC S t a b i l i t y and C o n t r o l Technique. AFFTC-TN-59-21, Edwards, C a l i f o r n i a , 1959.

F l e t c h e r , R.; and Powel l , M.J.D.: Comput. J.,

1977.

A Rap id l y Convergent Descent Method f o r M in im iza t i on . vo l . 6, no. 2, pp. 163-168, J u l y 1963.

C o n t r o l D e r i v a t i v e s . RAE TR 77009, 1977. Fos te r , G.W.: I d e n t i f i c a t i o n o f Hunter Mk 12 L o n g i t u d i n a l and L a t e r a l Aerodynamic S t a b i l i t y and

F o s t e r , G.W.: A D e s c r i p t i o n of t h e Weighted Leas t Squares Output E r r o r Method o f Parameter

Wind Tunnel C a l i b r a t i o n o f An A i r c r a f t P i t o t - s t a t i c and F l o w - D i r e c t i o n Measur ing Nose

I d e n t i f i c a t i o n . RAE TM FS 215, 1978.

F o s t e r , G.W.: Probe. RAE TR 80077, 1980.

5

F o s t e r , G.W.: The I d e n t i f i c a t i o n of A i r c r a f t S t a b i l i t y and C o n t r o l Parameters i n Turbulence. RAE TR 83025, 1982. C a l i f o r n i a , 1982.)

( A l s o a v a i l a b l e as Ph.D. Thesis , C a l i f o r n i a I n s i t u t e of Technology, Pasadena,

F r o i s y , J.B.: Smith, C.L.; C o r r i p i o , A.B.; and M u r r i l l , P.W.: Closed-Loop I d e n t i f i c a t i o n o f System Dynamics i n t h e Presence of Noise and Unmeasured D is tu rbances , Proc. 1 5 t h J o i n t Automat ic C o n t r o l Conference, Aus t i n , Texas, pp. 293-302, 1974.

European R o t o r c r a f t Forum, Paper 96, Stresa, I t a l y , September 13-15, 1983.

Mo t ion Used i n F r e e - F l i g h t and Wind Tunnel Data Reduct ion and Ana lys i s . NASA SP-3070, 1972.

T ranspor t A i r c r a f t . Dynamic S t a b i l i t y Parameters, AGARD-CP-235, Paper 18, 1978.

Guide Extens ion. Sp r inge r -Ver lag , B e r l i n , 1977. ( L e c t u r e notes i n Computer Science, 51.)

Fu, K.H.; and Marchand, M.: H e l i c o p t e r System I d e n t i f i c a t i o n i n t h e Frequency Domain. N i n t h

Gainer , Thomas G.; and Hoffman, Sherwood: Sumnary o f T rans fo rma t ion Equat ions and Equat ions o f

G a l b r a i t h , T.J.; and Petersen, T.J.: Non l i nea r Parameter I d e n t i f i c a t i o n and I t s A p p l i c a t i o n t o

Garbow, B.S.; Boy le, J.M.; Dongarra, J.J.; and Moler , C.B.: M a t r i x Eigensystem Rout ines - EISPACK

Garretson, H.C., 111: Beaver A i r c r a f t Parameter I d e n t i f i c a t i o n Techn ica l P repara t i ons and Techn ica l P repara t i ons and P r e l i m i n a r y Results. DFVLR-Mitt. 78-01, DEVLR I n s t i t u t F i i r Flugmechanik, Braunschweig, Federa l Republ ic o f Germany, J u l y 1978.

Garretson, H.C., 111: Beaver A i r c r a f t Parameter I d e n t i f i c a t i o n - T e c h n i c a l P repara t i ons and P r e l i m i n a r y Resu l t s . DFVLR-Mitt. 78-01, DELVR I n s t i t F i i r Flugmechanik, Braunschweig, Federa l Repub l i c o f Germany, Aug. 1978.

Sec t i ons ; a T r a n s l a t i o n of Theor ia Motus. T r a n s l a t e d and w i t h an Appendix by Char les Henry Davis i n 1857. Dover P u b l i c a t i o n s , New York, 1963.

Gauss, K a r l F r i e d r i c h : Theory of t h e Motion o f t h e Heavenly Bodies Moving About t h e Sun i n Conic

Ger lach, O.H.: De te rm ina t ion o f Performance, S t a b i l i t y and C o n t r o l C h a r a c t e r i s t i c s f rom Measurements

Ger lach, O.H.: D e t e r m i n a t i o n o f Performance and S t a b i l i t y Parameters f rom Nonsteady F l i g h t Test Maneu- vers. SAE N a t i o n a l Business A i r c r a f t Meeting, W i c h i t a , Kansas, SAE Paper 700236, March 18-20, 1970.

i n Non-Steady Manoeuvers. S t a b i l i t y and C o n t r o l , P a r t 1, AGARD-CP-17, pp. 499-523, Sept. 1966.

Ger lach, O.H.: The De te rm ina t ion o f S t a b i l i t y D e r i v a t i v e s and Performance C h a r a c t e r i s t i c s f rom Dynamic Manoeuvres. F l i g h t Test Techniques, AGARD CP-85, Paper 16, 1971.

Co., New York, 1967. Gessow, A l f r e d ; and Myers, Garry C.: Aerodynamics o f t h e H e l i c o p t e r . F r e d e r i c k Ungar P u b l i s h i n g

Geyser, L u c i l l e C.; and Leh t inen , Bruce: D i g i t a l Program f o r S o l v i n g t h e L i n e a r S t o c h a s t i c Opt imal C o n t r o l and E s t i m a t i o n Problem. NASA TN D-7820, Mar. 1975.

Gibson, J.C.: F l y i n g Q u a l i t i e s and t h e Fly-By-Wire Aeroplane. S t a b i l i t y and C o n t r o l , AGARD-CP-260, Paper 22, May 1979.

G i l l , P h i l i p E.; and Murray, Wa l te r : Non l i nea r Leas t Squares and N o n l i n e a r l y Cons t ra ined Op t im iza t i on . Dundee Conference on Numerical A n a l y s i s , 1975; Numerical Ana lys i s , pp. 134-147, Sp r inge r -Ver lag , B e r l i n , 1976. (Lec tu re Notes i n Mathematics, No. 506.)

G i l y a r d , Glenn B.: De te rm ina t ion o f Propulsion-System-Induced Forces and Moments o f a Mach 3 C r u i s e A i r c r a f t . Parameter E s t i m a t i o n Techniques and A p p l i c a t i o n i n A i r c r a f t F l i g h t Tes t i ng , NASA TN D-7647, pp. 369-374, 1974.

G i l y a r d , Glenn B.; and Be l te , Daumants: F l i gh t -De te rm ined Lag o f Ang le -o f -A t tack and A n g l e - o f - S i d e s l i p Sensors i n t h e YF-12A A i r p l a n e From Ana lys i s o f Dynamic Maneuvers. NASA TN D-7819, 1974.

(eds.), S t a t i s t i c a l Computation, pp. 365-397, Academic Press, New York, 1969.

Problems Whose V a r i a b l e s Separate. S I A M J. Numer. Anal., v o l . 10, no. 2, pp. 413-432, Apr. 1973.

Golub, G.H.: M a t r i x Decomposit ions and S t a t i s t i c a l C a l c u l a t i o n s . I n R.D. M i l t o n and John A. Ne lde r

Golub, G.H.; and Pereyra, V. : The D i f f e r e n t i a t i o n o f Pseudo-Inverses and Non l i nea r Leas t Squares

Goodson, R.E.; and P o l i s , M. (eds.): I d e n t i f i c a t i o n o f Parameters i n D i s t r i b u t e d Systems. Proc. J o i n t Automat ic C o n t r o l Conference, Austin, Texas, June 17-21, p. 155, 1974.

Goodwin, Graham C.: An Overview o f t h e System I d e n t i f i c a t i o n Problem - P a r t 4: Exper iment Design. S i x t h IFAC Symposium on I d e n t i f i c a t i o n and System Parameter Es t ima t ion , Washington, D.C., June 1982, s.4. 8 & q ~ 2nd G - ! . S.r idis, e& . , ?ergamon Press , Oxfordj 1983%

Ana lys i s . Academic Press, New York, 1977. Goodwin, Graham C.; and Payne, Robert L.: Dynamic System I d e n t i f i c a t i o n : Experiment Design and Data

6

Goodwin, G.C.; Payne, R.L.; and Murdoch, J.C.: Optimal Test S ignal Design f o r L i n e a r S i n g l e I n p u t - S i n g l e Output Closed Loop I d e n t i f i c a t i o n . U n i v e r s i t y o f Cambridge, I E E P u b l i c a t i o n No. 96, I n s t i t u t i o n o f E l e c t r i c a l Engineers, London, 1973.

He1 i c o p t e r f rom F1 i g h t Measurements. Na t iona l Research Counci l Canada, Ae ronau t i ca l Repor t LR-572, NRC-13882, Dec. 1973.

Conference on Computer Aided Con t ro l System Design,

Gould, D.G.; and Hindson, W.S.: Est imates o f t h e L a t e r a l - D i r e c t i o n a l S t a b i l i t y D r i v a t i v e s o f a

Gould, D.G.; and Hindson, W.S.: Est imates o f t h e S t a b i l i t y D e r i v a t i v e s o f a H e l i c o p t e r from F l i g h t Measurements. N i n t h Congress o f t h e I n t e r n a t i o n a l Counci l o f t h e Aeronau t i ca l Sciences, Ha i fa , I s raeq , Aug. 25-30, I G A S Paper 74-49, 1974.

Gould, D.G.; and Hindson, W.S.: A i r c r a f t f rom F1 i g h t Data. pp. 23-1 t o 23-9, May 1975.

Est imates o f t h e S t a b i l i t y D e r i v a t i v e s o f a H e l i c o p t e r and a V/STOL Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172,

Gracey. W i l l i a m : Measurement o f A i r c r a f t Speed and A l t i t u d e . NASA RP-1046, 1980.

Graupe. Danie l : On I d e n t i f y i n g S tochas t i c Closed-Loop Systems. IEEE Trans. Automat. C o n t r o l , V O ~ . AC-20, pp. 553-555, Aug. 1975.

Greenberg, Har ry :

Greenstadt . John: On t h e R e l a t i v e E f f i c i e n c i e s o f Grad ien t Methods. Math. Comp., v o l . 21, no. 99,

A Survey o f Methods f o r De te rm in ing S t a b i l i t y Parameters o f an A i r p l a n e from Dynamic F1 i g h t Measurements. NACA TN-2340, 1951.

pp. 360-367, J u l y 1967.

Grove, R.D.; Bowles. R.L.: and Mayhew, S.C.: A Procedure f o r E s t i m a t i n g S t a b i l i t y and Con t ro l Parameters f rom F l i g h t Test Data by Using Maximum L i k e l i h o o d Methods Employing a Real-Time D i g i t a l System. NASA TN D-6735, 1972.

Gupta, Narendra K.: New Frequency Domain Methods f o r System I d e n t i f i c a t i o n . Proc. J o i n t Automatic C o n t r o l Conference, San Franc lsco, June 22-24, 1977, v o l . 2, pp. 804-808. I n s t i t u t e o f E l e c t r i c a l and E l e c t r o n i c Engineers, New York, 1977.

Gupta, Narendra K.; and H a l l , W. E a r l , Jr.:

Gupta, Naren K.; and I l i f f , Kenneth W.: I d e n t i f i c a t i o n o f Aerodynamic I n d i c i a 1 Func t ions Using

Design and E v a l u a t i o n o f Sensor Systems f o r S t a t e and Parameter E s t i m a t i o n . J. Guid. C o n t r o l , vo l . 1, no. 6, pp. 397-403, Nov.-Dec. 1978.

F l i g h t Data. A I A A Paper 82-1375, Aug. 1982.

Gupta, N.K.; and Mehra, R.K: Computational Aspects o f Maximum L i k e l i h o o d E s t i m a t i o n and Reduc t ion i n S e n s i t i v i t y F u n c t i o n Ca lcu la t i ons . Dec. 1974.

I E E E Trans. Automat. C o n t r o l , v o l . AC-19, no. 6, pp. 774-783,

Gupta, Narendra K.; H a l l , W. E a r l , Jr.; and Trank le, Thomas L.: Advanced Methods o f Model S t r u c t u r e

Hafer , X.: Wind Tunnel Tes t i ng o f Dynamic D e r i v a t i v e s i n W. Germany. Dynamic S t a b i l i t y Parameters,

H a j d a s i n s k i , A.K.; Eykhof f , P.; Damen, A.A.H.; and van den Boom, A.J.W.:

De te rm ina t ion f rom Test Data. J. Guid. C o n t r o l , v o l . 1, no. 3, pp. 197-204, May-June 1978.

AGARD-CP-235, Paper 5, 1978.

D i f f e r e n t Model Sets f o r System I d e n t i f i c a t i o n . S i x t h IFAC Symposium on I d e n t i f i c a t i o n and System Parameter I d e n t i f i c a t i o n , Washington, D.C., June 7-11, 1982, pp. 47-55, Pergamon Press, Oxford and New York, 1983.

The Choice and Use of

H a l l , W.E.; and Bryson, A.E.: I n c l u s i o n o f R o t o r Dynamics i n C o n t r o l l e r Design f o r H e l i c o p t e r s . J. A i r c r a f t , v o l . 10, no. 4, pp. 200-206, Apr. 1973.

Hand l i ng O u a l i t i e s and S t a b i l i t y and C o n t r o l Eva lua t i on . P r e p r i n t No. 78-30, Proc. 34th Annual Forum o f t h e American H e l i c o p t e r Soc ie ty , Washington, D.C., May 1978.

I d e n t i f i c a t i o n f o r Nonl inear Aerodynamic F l i g h t Regimes. I d e n t i f i c a t i o n , AGARD-CP-172, Paper 21, 1974.

pp. 567-569, Nov.-Dec. 1970.

Aspects. Parameter I d e n t i f i c a t i o n , AGARD-LS-104, Paper 1, 1979.

Dynamic S t a b i l i t y Parameters, AGARD-LS-114, Paper 10, May 1981.

H a l l , W.E., Jr.; Gupta, N.K.; and Hansen, R.S.: R o t o r c r a f t System I d e n t i f i c a t i o n Techniques f o r

H a l l , W.E., Jr.; Gupta, N.K.; and T y l e r , J.S.: Model S t r u c t u r e De te rm ina t ion and Parameter Methods f o r A i r c r a f t S t a t e and Parameter

Hamel, P.G.: A Systems Analys is View o f Aerodynamic Coupl ing. J. A i r c r a f t , v o l . 7. no. 6,

Hamel, P.G.:

Hamel, P.G.:

A i r c r a f t Parameter I d e n t i f i c a t i o n Methods and T h e i r A p p l i c a t i o n s - Survey and F u t u r e

De te rm ina t ion of A i r c r a f t Dynamic S t a b i l i t y and C o n t r o l Parameters f rom F l i g h t Tes t i ng .

Hamel, P.G.; and Krag, B.: Dynamic Windtunnel S i m u l a t i o n o f A c t i v e Con t ro l Systems. S t a b i l i t y and I I C o n t r o l , AGARD-CP-260, Paper 16A. May 1979.

!

7

Her r i ng ton , R.M.; Shoemacher, R.E.; B a r t l e t t , E.P.; and Dunlap, E.W.: F l i g h t Test Eng ineer ing Handbook. AFFTC-TR-6273, Edwards, C a l i f o r n i a , AD-636392, Jan. 1966.

Hodge, Ward F.; and Bryan t , Wayne H.: Parameters Caused by Unmodeled F1 i g h t I ns t rumen ta t i on E r r o r s .

Hodgkinson, J.: LaManna, W.J.; and Heyde, J.L.: Augmentation Systems - A Fundamental Approach. Aeronaut. J., v o l . BO, no. 782, pp. 75-81, Feb. 1976.

Hohenemser, K.H.; Baner jee, D.; and Yin, S.K.: Ro to r Dynamic S t a t e and Parameter I d e n t i f i c a t i o n f rom Simulated Forward F l i g h t T rans ien ts . Part 1: NASA CR-137963: Pa r t 2: NASA CR-137964, June 1976.

Hohenemser, K.H.; and Banerjee, D.: f rom Simulated and Wind Tunnel Dynamic Test Data, Pa r t 2. NASA CR-152023, 1977.

Hohenemser, K.H.; and Crews, Sam T.: Tests , Pa r t 1. NASA CR-152022, 1977.

Monte C a r l o A n a l y s i s of I naccu rac ies i n Est imated A i r c r a f t NASA TN D-7712, 1975.

Hand l i ng Q u a l i t i e s o f A i r c r a f t w i t h S t a b i l i t y and Con t ro l

A p p l i c a t i o n o f System I d e n t i f i c a t i o n t o A n a l y t i c a l Ro to r Model ing

Unsteady Hover ing Wake Parameters I d e n t i f i e d f rom Dynamic Model

On t h e Use o f F i r s t Order Ro to r Dynamics i n M u l t i b l a d e Coord inates. Hohenemser, K.H.; and Yin, S.K.: P r e p r i n t No. 831, Proc. 30th Annual Nat ional Forum of t h e American H e l i c o p t e r Soc ie ty , Washington, D.C., May 7-9, 1974.

o f a Remotely P i l o t e d , Large-Scale ( 3 / 8 ) F i g h t e r A i r p l a n e Model. NASA TN D-8052, 1976.

Horsten, J.J.: Jonkers, H.L.; and Mulder, J.A.: F1 i g h t Test ing. Technische Hogeschool , D e l f t (Ne the r lands ) , Repor t LR-280, May 1979.

Hosman, R.J.A.W.: A Method t o D e r i v e Angle o f P i t ch , F l i g h t - P a t h Angle and Angle o f A t t a c k f rom Measurements i n Nonsteady F l i g h t . 1971.

Holleman, E u c l i d C.: S u n a r y o f F l i g h t Tests t o Determine t h e Spin and C o n t r o l l a b i l i t y C h a r a c t e r i s t i c s

F l i g h t Path Recons t ruc t i on i n t h e Context o f Nonsteady

Technische Hogeschool , D e l f t (Nether lands) , Repor t VTH-156, Apr.

Hosman, R.J.A.W.: Advanced F l i g h t Test I ns t rumen ta t i on : Design and C a l i b r a t i o n . Technische

Hosman, R.J.A.W.: Advanced F l i g h t Test I ns t rumen ta t i on : Design and C a l i b r a t i o n . Methods f o r A i r c r a f t

Howard, J.: The De te rm ina t ion o f L a t e r a l S t a b i l i t y and Con t ro l D e r i v a t i v e s from F l i g h t Data. Can.

Hsia, T ien C.: System I d e n t i f i c a t i o n : Least-Squares Methods. D.C. Heath and Co., Lex ington,

Huber, H.:

Huber, H.: E f f e c t o f Tors ion-Flap-Lag Coupl ing on H inge less Ro to r S t a b i l i t y . 29 th Annual N a t i o n a l Forum

I l i f f , Kenneth W.: I d e n t i f i c a t i o n and S tochas t i c Con t ro l w i t h A p p l i c a t i o n t o F l i g h t C o n t r o l i n

I l i f f , Kenneth W.:

Hogeschool , D e l f t (Nether1 ands), Repor t VTH-M-222, Oct. 1974.

S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 6, May 1975.

Ae ronau t i cs Space J., vo l . 13, no. 3, pp. 126-134, Mar. 1967.

Massachusetts, 1977.

Parametr ic Trends and Op t im iza t i on - P r e l i m i n a r y S e l e c t i o n o f C o n f i g u r a t i o n - P r o t o t y p e Design and Manufacture. H e l i c o p t e r Aerodynamics and Dynamics, AGARD-LS-63, Paper 7, Apr. 1973.

o f t h e American H e l i c o p t e r Soc ie ty , Washington, D.C., AHS R e p r i n t 731, May 9-11, 1973.

Turbulence. Ph.D. D i s s e r t a t i o n , Univ. o f C a l i f o r n i a , Los Angeles, May 1973.

J. A i r c r a f t , vo l . 14, no. 12, pp. 1175-1181, Dec. 1977.

C o n t r o l , vo l . 1, no. 2, pp. 101-108, Mar.-Apr. 1978 (a) .

Maximum L i k e l i h o o d Es t ima t ion o f L i f t and Drag f rom Dynamic A i r c r a f t Maneuvers.

Iliff, Kenneth W.: I d e n t i f i c a t i o n and S tochas t i c C o n t r o l o f an A i r c r a f t F l y i n g i n Turbulence. J. Guid.

I l i f f , Kenneth W.: E s t i m a t i o n of Aerodynamic C h a r a c t e r i s t i c s f rom Dynamic F l i g h t Test Data. Dynamic S t a b i l i t y Parameters, AGARD-CP-235, Paper 15, Nov. 1978 (b ) .

I l i f f , Kenneth W.: A i r c r a f t I d e n t i f i c a t i o n Experience. Parameter I d e n t i f i c a t i o n , AGARD-LS-104, Paper 6,

I l i f f , Kenneth W.; and Maine, R icha rd E.: P r a c t i c a l Aspects o f Using a Maximum L i k e l i h o o d Es t ima to r .

29 Oct.-2 NOV. 1979.

Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 16, May 1975.

Iliff, Kenneth W.; and Maine, Richard E.: F u r t h e r Observat ions on Maximum L i k e l i h o o d Es t ima tes o f S t a b i l i t y and C o n t r o l C h a r a c t e r i s t i c s Obtained f rom F l i g h t Data. A I A A Paper 77-1133, Hollywood, F l o r i d a , Aug. 1977.

Iliff, Kenneth W.; and Maine, R icha rd E.: NASA Dryden's Exper ience i n Parameter E s t i m a t i o n and I t s Use i n F l i g h t Test. AIAA Paper 82-1373, A I A A AFM Conference, San Diego, C a l i t o r n i a , k g . 1982.

Using a Newton-Raphson M i n i m i z a t i o n Technique. NASA TN D-6579, 1972. Iliff, Kenneth W.; and Tay lo r , Lawrence W.. Jr.: De te rm ina t ion o f S t a b i l i t y D e r i v a t i v e s f rom F l i g h t Data

8

I l i f f , Kenneth W.; Maine, R icha rd E.; and Shafer , Mary: Subsonic S t a b i l i t y and C o n t r o l D e r i v a t i v e s f o r an Unpowered, Remotely P i l o t e d 3 /8 -sca le F-15 A i r p l a n e Model Obta ined f r o m F l i g h t Test . 1976.

NASA TN D-8136,

I l i f f , Kenneth W.; Maine, R icha rd E.: and S tee rs , Sandra Thornberry : C o n t r o l C o e f f i c i e n t s o f t h e F-111A A i rp lane . NASA TM-72851, 1978.

F l i gh t -De te rm ined S t a b i l i t y and

I l i f f , Kenneth W.; Maine, R icha rd E.; and Montgomery, T.D.: Impor tan t Fac to rs i n t h e Maximum L i k e l i h o o d A n a l y s i s o f F l i g h t Test Maneuvers. NASA TP-1459, 1979.

I l i f f . Kenneth W.: Maine, R icha rd E.; and Cooke, Douglas R.: Se lec ted S t a b i l i t y and C o n t r o l D e r i v a t i v e s from t h e F i r s t Space S h u t t l e En t ry . Conference, Nov. 1981.

A I A A Paper 81-2451. AIAA/SETP/SFTE/SAE F i r s t F l i g h t T e s t i n g

Jategaonkar, Ravindra; and Plaetschke, Ermin:

Jazw insk i , Andrew H.: S tochas t i c Processes and F i l t e r i n g Theory. Academic Press, New York, 1970.

Maximum L i k e l i h o o d Parameter E s t i m a t i o n f r o m F l i g h t Test Data f o r General Non-Linear Systems. DFVLR-FB 83-14, AD-B076999, Apr. 1983.

Jeglum, P.M.: Parameters f rom Dynamic F l i g h t Test Maneuvers. Nov. 1978.

A i r Force F l i g h t Test Center Exper ience i n t h e I d e n t i f i c a t i o n o f S t a b i l i t y and C o n t r o l Dynamic S t a b i l i t y Parameters, AGARD-CP-235, Paper 14,

Johnston, D.E.: I d e n t i f i c a t i o n o f Key Maneuver -L im i t i ng F a c t o r s i n High-Angle-of -At tack F l i g h t . Dynamic S t a b i l i t y Parameters, AGARD-CP-235, Paper 36, Nov. 1978.

A p p l i c a t i o n o f t h e Kalman F i l t e r t o F l i g h t Path Recons t ruc t i on f rom F l i g h t T e s t Data Jonkers, H.L.: I n c l u d i n g E s t i m a t i o n o f I ns t rumen ta l B ias E r r o r Cor rec t i ons . Aerospace Eng ineer ing , D e l f t , Repor t VTH-162, 1976.

A i r c r a f t Systems and Technology Meeting, D a l l a s , Texas, A I A A Paper 76-897, Sept. 1976 (a) .

I n t e r n a t i o n a l Counc i l o f t h e Aeronau t i ca l Sciences, Ottawa, I C A S Paper 76-46, Oct. 1976 ( b ) .

D e l f t Technische Hogeschool, Department o f

Jonkers, H.L.; and Mulder, J.A.: New Developments and Accuracy L i m i t s i n A i r c r a f t F l i g h t Tes t i ng . A I A A

Jonkers, H.L.; and Mulder, J.A.: Accuracy L i m i t s i n Nonsteady F l i g h t Tes t i ng . Tenth Congress o f t h e

Jonkers, H.L.; Mulder , J.A.; and Horsten, J.J.: I n t r o d u c t i o n t o S t a t e Recons t ruc t i on o f Dynamic F l i g h t Test Manoeuvres. Contro l and Dynamic Systems, Advances i n Theory and A p p l i c a t i o n s , Vol. 21, C.T. Leondes, ed., Academic Press, New York, 1984.

Jonkers, H.L.; Mulder , J.A.; and Woerkom van, K.: Measurements i n Nonsteady F l i g h t : I n s t r u m e n t a t i o n and Ana lys i s . Proc. Seventh I n t e r n a t i o n a l Aerospace I n s t r u m e n t a t i o n Symposium, C r a n f i e l d , England, March 20-23. 1972, pp.21.1-21.10; Pe te r Peregr inus, Ltd., Stevonage, Her t s , 1972.

Joy, D.: A i r speed and D i r e c t i o n Measurement by Vor tex De tec t i on . A i r Data Symposium Proceedings, Naval Postgraduate School, Session I V : Hel icopter/VSTOL Sensors, Monterey, C a l i f o r n i a , June 1976.

Kaqiwada, H a r r i e t H.: System I d e n t i f i c a t i o n , Methods and A p p l i c a t i o n s . Addison-Wesley P u b l i s h i n g Co., Reading, Massachusetts; 1974.

K a i l a t h , Thomas: L i n e a r Systems. P r e n t i c e - H a l l , Inc., Englewood C l i f f s , New Jersey, 1980.

K a i l a t h , Thomas: Lectures on Wiener and Kalman F i l t e r i n g . New, Revised E d i t i o n . Sp r inge r -Ver lag , New York, 1981.

K a i l a t h , T.; and Lyung, L.: Asymptot ic Behav io r o f C o n s t a n t - C o e f f i c i e n t R i c c a t i D i f f e r e n t i a l Equat I E E E Trans. Automat. Contro l , vo l . AC-21, pp. 385-388, June 1976.

ons.

Ka le tka , J.: R o t o r c r a f t I d e n t i f i c a t i o n Experience. Parameter I d e n t i f i c a t i o n , AGARD-LS-104, Paper 7 , 1979.

Ka le tka , J.; and Langer, H.J.: C o r r e l a t i o n Aspects o f A n a l y t i c a l , Wind Tunnel and F l i g h t Test R e s u l t s f o r a H inge less R o t o r H e l i c o p t e r . 1982.

Group /F l i gh t Tes t Techniques and C o r r e l a t i o n , AGARD-CP-339, Paper 16,

Ka le tka , J.; and R ix , 0.: Aspects o f System I d e n t i f i c a t i o n o f H e l i c o p t e r s . T h i r d European R o t o r c r a f t and

Kalman, R.E.; and Bucy, R.S.: New R e s u l t s i n L i n e a r F i l t e r i n g and P r e d i c t i o n Theory. Trans. ASME,

Powered L i f t A i r c r a f t Forum, Aix-en-Provence, France, Paper 15, Sept. 1977.

Ser. D, J. B a s i c Eng., vol. 63, pp. 95-107, 1961.

Techniques. IEEE Trans. Automat. C o n t r o l , vo l . 16, no. 6, pp. 727-736, Dec. 1971. Kaminski, P.G.; Bryson, A.E.; and Schmidt, S.F.:

Kanning, G . ; and Biggers, J.C.:

Kashyap, R.L.:

D i s c r e t e Square Root F i l t e r i n g - A Survey of Cur ren t

A p p l i c a t i o n o f a Parameter I d e n t i f i c a t i o n Technique t o a H inge less H e l i c o p t e r Rotor . NASA TN 0-7834, 1974.

C o n t r o l , vo l . AC-15, no. 1, pp. 25-34, Feb. 1970. Maximum L i k e l i h o o d I d e n t i f i c a t i o n o f S t o c h a s t i c L i n e a r Systems. I E E E Trans. Automat.

9

K l e i n , V.: Parameter I d e n t i f i c a t i o n App l i ed t o A i r c r a f t . C r a n f i e l d Repor t Aero No. 26, C r a n f i e l d I n s t .

K l e i n , V.: L o n g i t u d i n a l Aerodynamic D e r i v a t i v e s o f a Slender Del ta-Wing Research A i r c r a f t E x t r a c t e d f rom

K l e i n , V.: On t h e Adequate Model f o r A i r c r a f t Parameter Es t ima t ion . C r a n f i e l d Repor t Aero No. 28,

K l e i n , V.: De te rm ina t ion of L o n g i t u d i n a l Aerodynamic D e r i v a t i v e s From Steady-State Measurement o f an

K l e i n , V.: A i r c r a f t Parameter E s t i m a t i o n i n Frequency Domain. A I A A Paper 78-1344, 1978.

K l e i n , V.:

o f Technology, 1974 (a) .

F l i g h t Data.

C r a n f i e l d I n s t . o f Technology, March 1975.

C r a n f i e l d Repor t Aero No. 27, CIT-FI-74-023, C r a n f i e l d I n s t . o f Technology, J u l y 1974 (b ) .

A i r c r a f t . A I A A Paper 77-1123, Hollywood, F l o r i d a , Aug. 1977.

De te rm ina t ion o f S t a b i l i t y and Contro l Parameters o f a L i g h t A i r p l a n e From F l i g h t Data Using Two E s t i m a t i o n Methods. NASA TP-1306, 1979.

K l e i n , V.: I d e n t i f i c a t i o n E v a l u a t i o n Methods. Parameter I d e n t i f i c a t i o n , AGARD-LS-104, Paper 2, 29 0ct.- 2 Nov. 1979.

K l e i n , V l a d i s l a v : Maximum L ike1 ihood Method f o r E s t i m a t i n g A i r p l a n e S t a b i l i t y and Con t ro l Parameters From F l i g h t Data i n Frequency Domain. NASA TP-1637, 1980.

K l e i n , V.; and Ba t te rson , J.G.: De te rm ina t ion o f A i r p l a n e Aerodynamic Parameters From F l i g h t Data a t High Angles o f A t tack . Proc. T h i r t e e n t h Congress o f t h e I n t e r n a t i o n a l Counci l o f t h e Aeronau t i ca l Sciences, v o l . I , B. Laschka and R. S t a u f e n b i e l , eds., pp. 467-474, American I n s t i t u t e o f Ae ronau t i cs and A s t r o n a u t i c s , New York, 1982.

K l e i n , V l a d i s l a v ; and Ba t te rson , James G.: Determinat ion o f A i r p l a n e Model S t r u c t u r e From F l i g h t Data

K l e i n , V l a d i s l a v ; and Ba t te rson , James G.: Aerodynamic C h a r a c t e r i s t i c s o f a F i g h t e r A i r p l a n e Determined

K l e i n , V.; and Keskar, A.D.: Frequency Domain I d e n t i f i c a t i o n o f a L i n e a r System Using Maximum L i k e l i h o o d Es t ima t ion . F i f t h IFAC Symposium on I d e n t i f i c a t i o n and System Parameter Es t ima t ion , Darmstadt, Sept. 1979. Pergaman Press, Oxford, 1980.

Equat ions and Extended Kalman F i l t e r . NASA TN D-8514, 1977.

Using Sp l i nes and Stepwise Regression. NASA TP-2126, 1983.

From F l i g h t and Wind Tunnel Data. NASA TP-2483, 1985.

K l e i n , V.; and Schiess, J.R.: C o m p a t i b i l i t y Check o f Measured A i r c r a f t Responses Using K inemat i c

K l e i n , V.; and Wi l l i ams , D.A.: On Some Problems Re la ted t o t h e I d e n t i f i c a t i o n o f A i r c r a f t Parameters. Proc. T h i r d IFAC Symposium on I d e n t i f i c a t i o n and System Parameter Es t ima t ion , The Hague, June 12-15, 1973, pp. 435-444, Nor th Hol land, Amsterdam, 1973.

K l e i n , V l a d i s l a v ; Ba t te rson , James G.; and Murphy, P a t r i c k C.: De te rm ina t ion o f A i r p l a n e Model S t r u c t u r e

K l e i n , V.; Ba t te rson , J.G.; and Smith, P.L.: On t h e De te rm ina t ion o f A i r p l a n e Model S t r u c t u r e From

From F l i g h t Data by Using M o d i f i e d Stepwise Regression. NASA TP-1916, Oct. 1981.

F l i g h t Data. S i x t h IFAC Symposium on I d e n t i f i c a t i o n and System Parameter Es t ima t ion , v o l . 2, George A. Bekey and George N. S a r i d i s , eds., pp. 1034-1039, Peragamon Press, Oxford, 1982.

K l e i n g e l d , H.W.: Design and E v a l u a t i o n o f a Symmetric F l i g h t Test Manoeuver f o r t h e E s t i m a t i o n of L o n g i t u d i n a l Performance and S t a b i l i t y and Con t ro l C h a r a c t e r i s t i c s . Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, pp. 9-1 t o 9-6, 1974.

K l o p f e n s t e i n , H.B.: Ob ta in ing A i r p l a n e Drag Data f rom Nonsteady F1 i g h t . A I A A Paper 65-211, 1965.

K l o s t e r , M.; Ka letka, J.; and Schaufele, H.: Parameter I d e n t i f i c a t i o n o f a H inge less R o t o r H e l i c o p t e r i n F l i g h t Cond i t i ons w i t h Increased I n s t a b i l i t y . S i x t h European R o t o r c r a f t and Powered L i f t A i r c r a f t Forum, B r i s t o l , England, Sept. 16-19, 1980, Conference Paper;, P a r t 2, U n i v e r s i t y o f B r i s t o l , B r i s t o l , 1980.

Koehler , R.; and Marchand, M.: Open/Closed Loop I d e n t i f i c a t i o n o f S t a b i l i t y and C o n t r o l C h a r a c t e r i s t i c s

Koeh le r , R.; and Wilhelm, K.: Auslegung von Eingangssignalen f i r d i e Kennwer te rm i t t l ung . I B 154-77/40,

Koehler , R.; and Wilhelm, K.: Closed Loop Aspects o f A i r c r a f t I d e n t i f i c a t i o n . Parameter I d e n t i f i c a t i o n ,

o f Combat A i r c r a f t . S t a b i l i t y and C o n t r o l , AGARD-CP-26D. Paper 16, May 1979.

DFVLR I n s t i t u t f i r Flugmechanik, Braunschweig, Federa l Repub l i c of Germany, Dec. 1977.

AGARD-LS-104, Paper 10. 29 Oct.-2 Nov. 1979.

Krag, B.: The Wind Tunnel Behaviour o f a Scaled Model w i t h a Gust A l l e v i a t i o n System i n a D e t e r m i n i s t i c Gust F i e i d . P r e p r i n t pp. 149-166, Nov. 1978 (a).

B russe ls , A c t i v e C o n t r o l Technology, The I n s t i t u t e , Rhode S t . Genese, Belg ium (Von Karman I n s t i t u t e f o r F l u i d Dynamics, L e c t u r e Ser ies 1978-1, ~ 0 1 . 2),

Symposium ijynamic Ana iys i s o f Venic ie i i i a e ana manoeuvring C h a r a c t e r i s t i c s . London,

Krag, B.: A c t i v e C o n t r o l Technology f o r Gust A l l e v i a t i o n . Von Karman I n s t i t u t e f o r F l u i d Dynamics,

Dec. 4-8, 1978 (b).

10

Kurz, H.; and Isermann, R.: Methods f o r On-Line Process I d e n t i f i c a t i o n i n Closed Loop. Proc. I n t e r - n a t i o n a l Federa t i on o f Automat ic Con t ro l S i x t h T r i e n n i a l World Congress, Boston and Cambridge, Massachusetts, Aug. 24-30, 1975, Pa r t 2, pp. 11.3 1 - 11.3 14. I ns t rumen t S o c i e t y o f America, P i t t s b u r g , 1975.

Ku rzha ls , P.R., ed.: Ac t i ve C o n t r o l s i n A i r c r a f t Design. AGARD-AG-234, Nov. 1978.

Kushner, H a r o l d J.: I n t r o d u c t i o n t o S tochas t i c Con t ro l . H o l t , R i n e h a r t and Winston, New York, 1971.

Kwakernaak. Huber t ; and Sivan, Raphael: L i n e a r Opt imal C o n t r o l Systems. Wi ley & Sons, New York, 1972.

L a i n i o t i - s , Demetrios G., ed.:

Lawson, Char les L.; and Hanson, R icha rd J.: S o l v i n g Least Squares Problems. P r e n t i c e - H a l l , Englewood C l i f f s , New Jersey, 1974.

F i f t h European R o t o r c r a f t and Powered L i f t A i r c r a f t Forum, Amsterdam, Nether lands, Sept. 1979.

E s t i m a t i o n Theory. American E l s e v i e r P u b l i s h i n g Co.. New York, 1974.

Langer, H.J.; and S t r i c k e r , R.: Some Resu l t s o f Dynamic Measurements wi th a Model Hingeless Ro to r .

Levad i , V i c t o r S.: Design o f I n p u t S igna ls f o r Parameter Es t ima t ion . IEEE Trans. Automat. C o n t r o l , v o l . 11, no. 2. pp. 205-211, 1966.

Levan, N.: Systems and S igna ls . O p t i m i z a t i o n Sof tware, Inc.. New York, 1983.

Lev in, M o r r i s J.: Optimal E s t i m a t i o n o f Impulse Response i n t h e Presence o f Noise. I R E Trans. C i r c u i t

L indberge r , N.A.: S tochas t i c M o d e l l i n g o f Computer-Regulated L i n e a r P l a n t s i n Noisy Environments. I n t .

L indberge r , N.A.: S tochas t i c I d e n t i f i c a t i o n o f Computer-Regulated L i n e a r P l a n t s i n Noisy Environments.

Theory, v o l . CT-7, no. 1, pp. 50-56, Mar. 1960.

J. C o n t r o l , vo l . 16, no. 6, pp. 1009-1019, 1972.

I n t . J. C o n t r o l , vo l . 17, no. 1, pp. 65-80, 1973.

L i p t s e r , Rober t S.; and Shi ryayev, A.N.: v o l . 1: General Theory, Spr inger-Ver lag, New York, 1977.

Litmann, S.; and Huggins. W.H.:

L i u s t e r n i k , Lazar A.; and Sobolev, V.J.: Elements o f F u n c t i o n a l Ana lys i s . T rans la ted f rom t h e Russian by A.E. Labarre, Jr., Herbe r t I z b i c k i , and H. Ward Crowley, F r e d e r i c k Ungar P u b l i s h i n g Co., New York, 1961.

S t a t i s t i c s o f Random Processes. T rans la ted by A.B. A r ies ,

Growing Exponen t ia l s as a P rob ing Signal f o r System I d e n t i f i c a t i o n . Proc. IEEE, vo l . 51, pp. 917-923, June 1963.

L jung, L.; Gustavsson, I.; and Soderstrom, T.: Under L i n e a r Feedback Con t ro l . IEEE Trans. Automat. C o n t r o l , v o l . AC-19, pp. 836-840, Dec. 1974.

Lobbia, R.N.; and Sar id i s , G.N.: On-Line I d e n t i f i c a t i o n o f M u l t i v a r i a b l e S tochas t i c Feedback Systems. T h i r t e e n t h J o i n t Automatic Con t ro l Conference, S tan fo rd , C a l i f o r n i a , Aug. 16-18, 1972, P r e p r i n t s o f Techn ica l Papers, pp. 802-810, American I n s t i t u t e o f A s t r o n a u t i c s , New York, 1972,

I d e n t i f i c a t i o n o f L inea r , M u l t i v a r i a b l e Systems Opera t i ng

Luenburger, David G.: O p t i m i z a t i o n by Vector Space Methods. John Wi ley & Sons, New York, 1969.

Luenberger, David G.:

Lumsden, R.B.:

Maine, R icha rd E.: Aerodynamic D e r i v a t i v e s f o r an Ob l i que Wing A i r c r a f t Est imated f rom F l i g h t Data by

User's Manual f o r SYNC, a FORTRAN Program f o r Merging and Time Synchron iz ing Data.

I n t r o d u c t i o n t o L i n e a r and Non l i nea r Programming. Addison-Wesley, Reading, Massachusetts, 1973.

Us ing an Automat ic Model Match ing Method. RAE TR 74103, 1974.

Using a Maximum L i k e l i h o o d Technique. NASA TP-1336, 1978.

NASA TM-81355, 1981 (a).

Parameter Es t ima t ion . NASA TP-1690, 1981 (b).

C o n t r o l D e r i v a t i v e s From F l i g h t Data. NASA TN D-7831, 1975.

D e r i v a t i v e s f rom F l i g h t Data. J. A i r c r a f t , v o l . 16, no. 10, pp. 674-679, Oct. 1979.

L i k e l i h o o d Parameter Es t ima t ion . NASA TP-1563, 1980.

Es t ima t ion o f L o n g i t u d i n a l Aerodynamic D e r i v a t i v e s o f t h e Comet 3B f rom F l i g h t Test Data

Maine, Richard E.:

Maine, R icha rd E.: Programmer's Manual f o r MMLE3, A General FORTRAN Program f o r Maximum L i k e l i h o o d

A FORTRAN Program f o r De te rm in ing A i r c r a f t S t a b i l i t y and

Maximum L i k e l i h o o d E s t i m a t i o n o f T r a n s l a t i o n a l A c c e l e r a t i o n

Maine, R icha rd E.; and I l i f f , Kenneth W.:

Maine, R icha rd E.; and I l i f f , Kenneth W.:

Maine, R icha rd E. ; and I l i f f , Kenneth W.; Use r ' s Manual f o r MMLE3, A General FORTRAN Program f o r Maximum

Maine, R icha rd E.; and I l i f f , Kenneth W.: Fo rmu la t i on and Implementat ion o f a P r a c t i c a l A l g o r i t h m f o r Parameter E s t i m a t i o n w i t h Process and Measurement Noise. S I A M J. Appl. Math., vo l . 41, no. 3, pp. 558-579, Dec. 1981 (a ) .

I

I

11

Maine, R icha rd E.; and I l i f f , Kenneth W.: The Theory and P r a c t i c e o f E s t i m a t i n g t h e Accuracy o f Dynamic F l i gh t -De te rm ined C o e f f i c i e n t s . NASA RP-1077, 1981 (b) .

Maine, R icha rd E.; and I l i f f , Kenneth W.: I d e n t i f i c a t i o n o f Dynamic Systems. AGARD-AG-300, 1984.

Maine, R icha rd E.; and I l i f f , Kenneth W.: A p p l i c a t i o n o f Parameter E s t i m a t i o n t o A i r c r a f t S t a b i l i t y and C o n t r o l - T h e Ou tpu t -E r ro r Approach. NASA RP-1168, 1986.

Marchand, M.: Der E i n f l u s s von Messfehlern auf d i e Bes t imnbarke i t de r Kennwerte d e r Lbngsbewegung.

Untersuchung der Bestimmbarkeit d e r f lugmechanischen D e r i v a t i v e des CCV-Versuchst r lgers

DFVLR IB 154-74/31, 1974.

Marchand, M.: F-104 G. IB 154-77/12, DFVLR I n s t i t u t fib Flugmechanik, Braunschweig, Federa l Repub l i c of Germany, Mar. 1977.

Marchand, M.; and Fu, K.-H.: Frequency Domain Parameter E s t i m a t i o n o f Ae ronau t i ca l Systems Wi thou t and Wi th Time Delay. Seventh IFAC/IFORS Symposium on I d e n t i f i c a t i o n and System Parameter Es t ima t ion , York, England, J u l y 3-7, 1985.

and Frequency Response Methods. pp. 17-1 t o 17-18, May 1975.

Margason, R.J.; and Lamar, J.B.: C h a r a c t e r i s t i c s o f Complex P1 anforms. NASA TN D-6142, 1971.

Marchand, M.; and Koehler , R.: De te rm ina t ion of A i r c r a f t D e r i v a t i v e s by Automat ic Parameter Adjustment Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172,

Vortex L a t t i c e FORTRAN Program f o r E s t i m a t i n g Subsonic Aerodynamic

Marquardt , Donald W.: An A l g o r i t h m f o r Least Squares E s t i m a t i o n o f Non l i nea r Parameters. J. SIAM,

Marquardt , Donald W.: Genera l ized Inverses, Ridge Regression, B iased L i n e a r Es t ima t ion , and Non l i nea r

Matheny, N e i l W.; and Pangeas, George N.: HiMAT Aerodynamic Design and F l i g h t Test Experience. A I A A

McCracken, J.R.; Ka le tka , J.; Meyer. H.; R ix , 0.; and Gartung, E.: CASA C-212 F l i g h t Test and Parameter I d e n t i f i c a t i o n . Spain-Federal Repub l i c o f Germany Coopera t i ve Research Program, DFVLR IB 154-76/16, 1976.

V O ~ . 11, pp. 431-441, 1963.

E s t i m a t i o n . Technometrics, vo l . 12, no. 3, pp. 591-612, Aug. 1970.

Paper 81-2433, Nov. 1981.

McLaren, I.: F l i g h t Test I n s t r u m e n t a t i o n Series, Open and Closed Loop Accelerometers. AGARD-AG-160,

Medi tch, J. S.: S t o c h a s t i c Optimal L i n e a r Es t ima t ion and C o n t r o l . McGraw-Hil l Book Co., New York. 1969.

Mehra, R.K.: I d e n t i f i c a t i o n o f S t o c h a s t i c L inear Dynamic Systems Using Kalman F i l t e r Represen ta t i on .

v o l . 6, J u l y 1974.

A I A A J., vo l . 9, no. 1, pp. 28-31. Jan. 1971.

Mehra, R.K.: Optimal I n p u t s f o r L i n e a r System I d e n t i f i c a t i o n . T h i r t e e n t h J o i n t Automat ic Con t ro l Conference, Stanford, C a l i f o r n i a , Aug. 16-18, 1972, P r e p r i n t s o f Technica l Papers, pp. 811-820, American I n s t i t u t e o f Ae ronau t i cs and As t ronau t i cs , New York, 1972.

Mehra, R.K.: I d e n t i f i c a t i o n i n Con t ro l and Econometrics; S i m i l a r i t i e s and D i f f e r e n c e s . D i v i s i o n o f Eng ineer ing and App l i ed Phys ics, Harvard U n i v e r s i t y , Cambridge, Massachusetts, Technica l Repor t 647, AD-767393, 1973.

Mehra, R.K.: Frequency-Domain Synthes is o f Optimal I n p u t s f o r L i n e a r System Parameter Es t ima t ion . D i v i s i o n o f Eng ineer ing and App l i ed Physics, Harvard U n i v e r s i t y , Cambridge, Massachusetts, Technica l Repor t 645, J u l y 1973. ( A l s o pub l i shed i n ASME Trans. Ser. G, J. Dynamic Systems, Measurement and C o n t r o l , v o l . 98, June 1976, pp. 130-138. ASME Paper 76-AUT-V.)

Mehra, R.K.:

Mehra, R.K.; and Gupta, N.K.: S ta tus o f I npu t Des ign f o r A i r c r a f t Parameter I d e n t i f i c a t i o n . Methods f o r

Mehra, Raman K.; and L a i n i o t i s , D i m i t r i G. (eds.): System I d e n t i f i c a t i o n : Advances and Case Studies.

Mendel, J e r r y M.: D i s c r e t e Techniques o f Parameter E s t i m a t i o n : The Equat ion E r r o r Fo rmu la t i on . Marcel

Mo le r , C.B.; and Stewart , G.W.: An A l g o r i t h m f o r Genera l i zed M a t r i x E igenvalue Problems. SIAM J. Numer.

Mo le r , Cleve; and Van Loan, Char les: Nineteen Dubious Ways t o Compute t h e Exponen t ia l o f a M a t r i x . SIAM

Optimal I n p u t S i g n a l s f o r Parameter E s t i m a t i o n i n Dynamic Systems, Survey and New Resu l t s . IEEE Trans. Automat. C o n t r o l , vo l . AC-19, no. 6, pp. 753-768, Dec. 1974.

A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 12, May 1975.

Academic Press, New York, 1976.

Dekker, Inc., New York, 1973.

Anai., voi . lo, no. 2, pp. 241-256, Apr. 1973.

Rev., v o l . 20. no. 4, pp. 801-836, kt. 1978.

I

12

Mo lus i s , J.A.: H e l i c o p t e r S t a b i l i t y D e r i v a t i v e E x t r a c t i o n and Data P rocess ing Us ing Kalman F i l t e r i n g Techniques. 28th Annual N a t i o n a l Forum o f t h e American H e l i c o p t e r Soc ie ty , Washington, D.C., May 17-19, 1972. AHS P r e p r i n t No. 641, 1972.

Mo lus i s , J.A.: A n a l y t i c a l Study t o D e f i n e a H e l i c o p t e r S t a b i l i t y D e r i v a t i v e E x t r a c t i o n Method, V O ~ . 1:

H e l i c o p t e r S t a b i l i t y D e r i v a t i v e E x t r a c t i o n f rom F l i g h t Data Us ing t h e Bayesian Approach

R o t o r c r a f t D e r i v a t i v e I d e n t i f i c a t i o n f rom A n a l y t i c a l Models and F l i g h t Test Data.

F i n a l Repor t . NASA CR-132371, 1973.

Mo lus i s , J.A.: t o Es t ima t ion . J. Am. H e l i c o p t e r SOC., v o l . 18, no. 2, pp. 12-23, Apr. 1973.

M o l u s i s , J.A.:

Mulder , J.A.: A i r c r a f t Performance Measurements i n Nonsteady F l i g h t s . Proc. T h i r d I n t e r n a t i o n a l

R o t o r c r a f t Parameter I d e n t i f i c a t i o n , Session V, AGARD-CP-172, Paper 24, May 1975.

F e d e r a t i o n o f Automatic Con t ro l Symposium on I d e n t i f i c a t i o n and System Parameter Es t ima t ion , P a r t 2, D e l f t , The Hague, pp. 1131-1145, June 12-15, 1973.

Flugzengkenndaten ans Flugverschen, DLGR-Mitt-73-25 und Raumfahrt, Cologne, 1973. De te rm ina t ion o f A i r c r a f t C h a r a c t e r i s t i c s From F l i g h t Tests , European Space Agency, P a r i s , pp. 171-190, Nov. 1974.

Mulder , J.A.: Some Aspects o f Performance Measurements i n Non-steady F l i g h t . Bestimming Von ( T r a n s l a t e d as

Mulder , J.A.: Es t ima t ion o f t h e A i r c r a f t S t a t e i n Non-steady F l i g h t . Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 19, May 1975.

Mulder , J.A.: Es t ima t ion o f Th rus t and Drag i n Non-steady F l i g h t . Proc. F o u r t h I n t e r n a t i o n a l F e d e r a t i o n o f Automat ic C o n t r o l Symposium on I d e n t i f i c a t i o n and System Parameter Es t ima t ion , T b i l i s i , Georgian, USSR, Sept. 21-27, 1976.

Mulder , J.A.: The Measurement o f Performance, S t a b i l i t y and C o n t r o l C h a r a c t e r i s t i c s o f a High Subsonic J e t A i r c r a f t i n Non-steady F l i g h t Cond i t i ons Employing High Accuracy I n s t r u m e n t a t i o n Techniques. Aeronaut. J., vo l . 81, pp. 247-258, June 1977.

Mulder , J.A.; and den Hol lander , J.G.: S t a t u s of Dynamic F l i g h t Test Technology - Model I d e n t i f i c a t i o n f o r F l i g h t S imulat ion. Apr. 1981. ( A l s o publ ished i n Trans. SAE, Sept. 1982.

SAE Business A i r c r a f t Meet ing and E x p o s i t i o n , W ich i ta , Kansas, SAE Paper 810597,

Mulder , J.A.; and Hosman, R.J.A.W.: The A p p l i c a t i o n o f High Accuracy I n s t r u m e n t a t i o n Techniques t o A i r c r a f t F l i g h t Testing. She l l A v i a t i o n News, no. 425, 1974.

Mulder , J.A.; and van S l i e d r e g t , J.M.: E s t i m a t i o n o f Drag and Th rus t o f J e t - p r o p e l l e d A i r c r a f t by

Mulder , J.A.; Jonkers, H.L.; Horsten, J.J.; Breeman, J.H.; and Simons, J.H.: Ana lys i s o f A i r c r a f t

Nonsteady F l i g h t Test Maneuvers. AGARD-CP-222, pp. 11-1 t o 11-30, 1977.

Performance, S t a b i l i t y and C o n t r o l Measurements, P a r t I : T h e o r e t i c a l Aspects i n Parameter I d e n t i c a t i o n . Parameter I d e n t i f i c a t i o n , AGARD-LS-104, 1979.

Mulder , J.A.; den Hol lander , J.G.; and B i n k h o r s t , H.: Aerodynamic Model I d e n t i f i c a t i o n f rom Dynamic F l i g h t Test Data and Wind Tunnel Experiments. AGARD-CP-339, Paper 14, Jan. 1983. Technische Hogeschool, D e l f t , Nether lands, Oct. 1982.)

I E E E Conference on Decis ion and Con t ro l , Miami Beach, F l o r i d a , Dec. 15-17, 1971, IEEE, New York,

Ground/Fl i g h t T e s t Techniques and CorrelaJiion, ( A l s o p u b l i s h e d as Repor t VLR-361, D e l f t U n i v e r s i t y o f Technology,

Nahi, N.E.; and Napjus, G.A.: Design o f Opt imal P rob ing S i g n a l s f o r Vec to r Parameter Es t ima t ion . Proc.

pp. 162-168, 1971.

Nahi, N.E.; and W a l l i s , D.E., Jr.: Opt imal I n p u t s f o r Parameter E s t i m a t i o n i n Dynamic Systems w i t h Whi te Observa t i on Noise. Tenth American Automat ic Con t ro l Counc i l J o i n t Automat ic C o n t r o l Conference, U n i v e r s i t y o f Colorado, Boulder , Colorado, P r e p r i n t s o f Techn ica l Papers, pp. 506-513, Aug. 5-7, 1969.

Ner ing, Evar D.: L inea r A lgebra and M a t r i x Theory. Second ed. John Wi ley & Sons, New York, 1970.

Neveu, Jacques: Mathematical Foundat ions o f t h e Ca lcu lus o f P r o b a b i l i t y . Holden-Day, Inc., San

Nguyen, Lua t T.; G i l b e r t , W i l l i a m P.; Gera, Joseph; I l i f f . Kenneth W.; and Enevoldson, E i n a r K.: A I A A

F ranc i sco , 1965.

A p p l i c a t i o n o f High-Alpha Con t ro l System Concepts t o a Variable-Sweep F i g h t e r A i rp lane . Atmospheric F l i g h t Mechanics Conference, Danvers, Massachusetts, Aug. 11-13, 1980, A I A A Paper 80-1582. 1980.

N ipp ress , K.R.: Performance E s t i m a t i o n f rom Non-Steady Maneuvers. F i r s t A I A A , SETP, SFTE, SAE, I T E A and I E E E F l i g h t T e s t i n g Conference, Las Vegas, Nevada, Nov. 11-13, 1981, A I A A Paper 81-2424, 1981.

Nor ton, Har ry N.:

Dgata, Ka tsuh iko : Modern C o n t r o l Engineer ing. P r e n t i c e - H a l l , Englewood C l i f f s , New Jersey, 1970.

O'Leary, C.O.:

Handbook of Transducers f o r E l e c t r o n i c Measur ing Systems. P r e n t i c e H a l l , Englewood C l i f f s , New Jersey, 1969.

Wind-Tunnel Measurement o f L a t e r a l Aerodynamic Derivatives Us ing a New O s c i l l a t o r y R i g and Comparisons f o r a Gnat A i r c r a f t . RAE TR 77159, 1977.

13

Oppenheim, A.V.; and Shafer , R.W.: D i g i t a l S ignal Processing. P r e n t i c e - H a l l , Englewood C l i f f s ,

Or l i k -Rkkemann , K.J.: Aerodynamic Coupl ing between L a t e r a l and L o n g i t u d i n a l Degrees o f Freedom. A I A A

Or l i k -Rkkemann . K.J.:

New Jersey, 1975.

J., vo l . 15, no. 12, pp. 1792-1799, Dec. 1977.

Parameters, AGARD-CP-235, Paper 1, 1978.

C o l l e g e P u b l i s h i n g , Lex ing ton , Massachusetts, 1974.

Automat ion and Remote C o n t r o l , vo l . 34, no. 9, p t . 2, pp. 1457-1466, Feb. 15, 1974.

Techniques f o r Dynamic S t a b i l i t y T e s t i n g i n Wind Tunnels.

Paige, Lowe l l J.; S w i f t , J. Dean; and Slobko, Thomas A.: Elements o f L i n e a r Algebra. Second ed. Xerox

Panich, Yu. V.; and T r a c h e v s k i i , M.L.: I d e n t i f i c a t i o n o f a Class o f Closed-Loop C o n t r o l Systems.

Papou l i s , Athanasios: P r o b a b i l i t y , Random Var iab les, and S t o c h a s t i c Processes. McGraw-Hil l Book Co.,

Dynamic S t a b i l i t y

New York, 1965.

Park, Gary D.: De te rm ina t ion o f T a i l - O f f A i r c r a f t Parameters, Systems I d e n t i f i c a t i o n . Proc. A I A A T h i r d Atmospher ic F l i g h t Mechanics Conference, A r l i n g t o n , Texas, pp. 128-136, June 7-9, 1976.

J. A i r c r a f t , vo l . 14, pp. 251-256, March 1977. Park, Gary D.: Parameter I d e n t i f i c a t i o n Technology Used i n De te rm in ing I n - F l i g h t A i r l o a d Parameters.

Penrose, R.: A Genera l i zed Inve rse f o r Matr ices. Proc. Cambridge P h i l o s o p h i c a l S o c i e t y 51, p t . 3,

Pe rk ins , Cour t l and D.; and Hage, Rober t E.: A i r p l a n e Performance S t a b i l i t y and C o n t r o l . John Wi ley &

Pitman, Edwin. J.G.: Some Bas ic Theory f o r S t a t i s t i c a l In ference. Chapman and H a l l , London, 1979.

P laetschke, E.: Parameter I d e n t i f i c a t i o n : I t s Purpose, Methods, and R e s u l t i n g Requirements f o r F l i g h t Tes t I ns t rumen ta t i on . AGARD/Cranfield/DFVLR Shor t Course on F l i g h t Test I n s t r u m e n t a t i o n , 1977.

P laetschke, E.; and Schulz , G.: P r a c t i c a l Input S igna l Design. Parameter I d e n t i f i c a t i o n , AGARD-LS-104, Paper 3, 29 Dct.-2 Nov. 1979.

P laetschke, E.; Mulder, J.A.; and Breeman, J.H.: F l i g h t Test R e s u l t s o f F i v e I n p u t S i g n a l s f o r A i r c r a f t Parameter I d e n t i f i c a t i o n . Proc. S i x t h IFAC Symposium on I d e n t i f i c a t i o n and System Parameter E s t i m a t i o n , Washington, D.C., Jan. 7-11, 1982, vol. 2, pp. 1149-1154, Pergamon Press, Oxford and New York, 1983.

P laetschke, E.; Mulder. J.A.; and Breeman, J.H.: R e s u l t s o f Beaver A i r c r a f t Parameter I d e n t i f i c a t i o n .

pp. 406-413, 1955.

Sons, New York, 1949.

DFVLR-FB 83-10, 1983.

Polak, E l i j a h : Computat ional Methods i n Op t im iza t i on : A U n i f i e d Approach. Academic Press, New York, 1971.

Poo l , A.; and Bosman, D . : Bas ic P r i n c i p l e s o f F l i g h t Test I n s t r u m e n t a t i o n Engineer ing. AGARD F l i g h t T e s t I n s t r u m e n t a t i o n Ser ies , AGARD-AG-160, vol. 1, 1974.

P o t t e r , James E.: M a t r i x Quadt-at ic Solut ions. S I A M J. Appl. Math., vo l . 14, no. 3, pp. 496-501, May 1966.

P o u l t e r , R.L.: Measurement o f t h e Yawing Moment o f I n e r t i a o f an A i r c r a f t (HP 115) i n F l i g h t . RAE A.R.C. R. & M. 3691, 1972.

Pouwels, H.: I n s t r u m e n t a t i o n f o r t h e Determinat ion o f A i r c r a f t Performance f rom Dynamic Maneuvers. Proc. 2 5 t h I n t e r n a t i o n a l I n s t r u m e n t a t i o n Symposium, Anaheim, C a l i f o r n i a , May 7-10, 1979, P a r t 2, pp. 611-621, Ins t rumen t S o c i e t y o f America, 1979.

C a l c u l a t i n g D e r i v a t i v e s .

Parameter and S t a t e I d e n t i f i c a t i o n . 11th American Automat ic C o n t r o l Counci l , J o i n t Automat ic C o n t r o l Conference, Georg ia I n s t i t u t e o f Technology, A t l a n t a , June 22-26, 1970, Paper 18-G, pp. 449-450, American S o c i e t y o f Mechanical Engineer ing, New York, 1970.

Powel l , M.J.D.: An E f f i c i e n t Method f o r F ind ing t h e Minimum o f a F u n c t i o n o f Severa l V a r i a b l e s Wi thou t Comput. J., vo l . 7, no. 2, pp. 155-162, J u l y 1974.

Powel l , J. David; and T y l e r , James S. , Jr.: A p p l i c a t i o n o f t h e Kalman F i l t e r and Smoothing t o VTOL

Powers, Bruce G.: Phugoid C h a r a c t e r i s t i c s o f a YF-12 A i r p l a n e Wi th Variable-Geometry I n l e t s Obta ined i n F l i g h t T e s t s a t a Mach Number o f 2.9.

IEEE Trans. Automat. C o n t r o l , vo l . AC-22, no. 6, pp. 987-988, Dec. 1977.

NASA TP-1107, 1977.

Prasad, R.M.; Sinha, A.K.; and Mahalanabis, A.K.: Two-Stage I d e n t i f i c a t i o n o f Closed-Loop Systems.

P r i e s t l e y , M.B.: E s t i m a t i o n o f T r a n s f e r Funct ions i n Closed Loop S t o c h a s t i c Systems. A u t m a t i c a , vo l . 5, no. 5, pp. 623-632, Sept. 1969.

1 4

Ramachandran, S.; Schneider, H.; Mason, J.D.; and S t a l f o r d , H.L.: I d e n t i f i c a t i o n o f A i r c r a f t Aerodynamic C h a r a c t e r i s t i c s a t High Angles o f A t t a c k and S i d e s l i p Us ing t h e E s t i m a t i o n Before M o d e l l i n g (EBM) Technique. A I A A Paper 77-1169. 1977.

F i g h t e r A i r c r a f t from F l i g h t Data. A I A A Paper 74-790, 1974. Ramachandran, S.: and Wells, W.R.: E s t i m a t i o n o f N o n l i n e a r Aerodynamic D e r i v a t i v e s o f a V a r i a b l e Geometry

De te rm ina t ion o f S t a b i l i t y D e r i v a t i v e s from F l i g h t Tes t Data by Rampy, John M.; and Berry, Donald T.:

Rao, C.R.: L i n e a r S t a t i s t i c a l I n f e r e n c e and I t s A p p l i c a t i o n s . John Wi ley Sons, New York, 1965.

Rao, S . S . : Opt im iza t i on , Theory and A p p l i c a t i o n s . W i ley Eas te rn L i m i t e d , New D e l h i , 1978.

R e i c h e r t , G.: B a s i c Dynamics o f Rotors : Con t ro l and S t a b i l i t y of Ro ta ry Wing A i r c r a f t : Aerodynamics H e l i c o p t e r Aerodynamics, AGARD-LS-63, Paper 3,

Means o f High Speed R e p e t i t i v e Opera t i on Analog Matching. FTC-TDR-64-8, Edwards, C a l i f o r n i a , May 1964.

and Dynamics o f Advanced Rotary-wing Con f igu ra t i ons . Apr. 1973.

Re id , G.E.A.: V a l i d a t i o n o f K inemat ic C o m p a t i b i l i t y o f F l i g h t Data Us ing Parameter E s t i m a t i o n Methodology. R A E TR 81020, Mar. 1981.

Reid, G.E.A.: I d e n t i f i c a t i o n o f t h e Aerodynamic S t a b i l i t y and C o n t r o l D e r i v a t i v e s o f an Unpowered

Renz, Ronald R.L.; Clarke, Rober t ; Mosser, Mark A.; Roskam, Jan; and Rummer, Dale: Development o f a

F r e e - F l i g h t A i r c r a f t Model. RAE TR 81146, Jan. 1981.

Simple, Se l f - con ta ined F l i g h t Test Data A c q u i s i t i o n System. E x p o s i t i o n , W ich i ta , Kansas, A p r i l 7-10, 1981, SAE Paper 810596, 1981.

SAE Business A i r c r a f t Meet ing and

R i x , 0.; and Hanke, D.: I n - F l i g h t Measured C h a r a c t e r i s t i c s o f Combined F l a p - S p o i l e r D i r e c t L i f t Con t ro l s . Aerodynamic C h a r a c t e r i s t i c s o f Con t ro l s , AGARD-CP-262, Paper 16, Sept. 1979.

33rd Annual Forum o f t h e American H e l i c o p t e r Soc ie ty , Washington, D.C., May 9-11, AHS 77-33-42, 1977.

Regelungstechnik und Prozess Datenverarbei tung, vo l . 22, pp. 282-283, 1974.

R ix , 0.; Huber, H.; and Kaletka,-J.: Parameter I d e n t i f i c a t i o n o f a H inge less Ro to r H e l i c o p t e r . Proc.

RSdder, P.: S t a t i s t i s c h e r F e h l e r b e i d e r S y s t e m i d e n t i f i z i e r u n g i m geschlossenen Rege lk re i s .

Rosenbrock, H.H.: An Automatic Method f o r F i n d i n g t h e Grea tes t o r Least Value o f a Func t i on . Comput. J. .

Ross, A. Jean: De te rm ina t ion o f Aerodynamic D e r i v a t i v e s From T r a n s i e n t Responses i n Manoeuvring F l i g h t .

V O ~ . 3., pp. 175-184, 1960.

Tehn ica l Memorandum Aero 1598, Royal A i r c r a f t Es tab l i shmen t , 1974. ( A l s o pub l i shed i n Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, May 1975.)

De te rm ina t ion o f Aerodynamic D e r i v a t i v e s f rom T r a n s i e n t Response i n Manoeuvring F l i g h t . Ross, A. Jean. Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 14, 1974.

Ross, A. Jean: A p p l i c a t i o n o f Parameter I d e n t i f i c a t i o n Techniques t o t h e A n a l y s i s o f F l i g h t Data. Prog.

Ross, A. Jean:

Aerospace Sciences, vol. 18, no. 4, pp. 325-349, 1979.

AGARD-LS-104, Paper 8, Nov. 1979.

Tests . RAE TR 80099, 1980.

I d e n t i f i c a t i o n Exper ience i n Extreme F l i g h t Regimes. Parameter I d e n t i f i c a t i o n ,

Ross, A. Jean: Revised Values o f t h e L a t e r a l Aerodynamic D e v i a t i o n s o f t h e Gnat A i r c r a f t From F l i g h t

Ross, A. Jean; and Foster, G.W.: F o r t r a n Programs f o r t h e D e t e r m i n a t i o n o f Aerodynamic D e r i v a t i v e s From T r a n s i e n t L o n g i t u d i n a l o r L a t e r a l Responses o f A i r c r a f t . RAE ARC CP-1344, 1976.

Ross, A.J.; and Thomas, H.H.B.M.: A Survey o f Exper imenta l Data on t h e Aerodynamics o f C o n t r o l s i n t h e L i g h t o f F u t u r e Needs. Aerodynamic C h a r a c t e r i s t i c s o f Con t ro l s . AGARD-CP-262, Paper 2, Sept. 1979.

Ross, A. Jean; Fos te r , G.W.; and Turvey. T.: An I n v e s t i g a t i o n o f Dutch R o l l and Wing Rock O s c i l l a t i o n s o f a Gnat T r a i n e r A i r c r a f t : F l i g h t Tes ts and L i n e a r A n a l y s i s . RAE TR 78032, Mar. 1978.

R o t i e r , D.J.; and F e r r i n , F.J.: U l t r a s o n i c Wind Vec to r Sensor. A i r Data Symposium Proceedings, Naval Postgraduate School, Monterey, C a l i f o r n i a , Session V: Helicoper/VSTOL Sensors, June 1976.

Royden, H.L.: Real Analys is . Second ed. MacMi l lan, London, 1968.

Rudin, Wa l te r : Real and Complex Ana lys i s . Second ed. McGraw-Hi l l . New York, 1974.

Rynaski , Edmund G.; Andr isani , Dominick, 11; and Weingarten, Norman C.: I d e n t i f i c a t i o n o f t h e S t a b i l i t y

E s t i m a t i o n Theory w i t h A p p l i c a t i o n t o Comnunications and Con t ro l .

Parameters o f An A e r o e l a s t i c A i rp lane . A I A A Paper 78-1328, Aug. 1978.

McGraw-Hil l , New York, 1971. Sage, Andrew P.; and Melsa, James L.:

15

Sage, Andrew P.; and Melsa, James L.: System I d e n t i f i c a t i o n . Academic Press, New York, 1971.

Schmidt, E.: Die AVA-Derivativwaage. DLR-Mitt-74-32, J u l y 1974.

Schuetz. A.J.: Low Angle-of -At tack Long i tud ina l Aerodynamic Parameters o f Navy T-2 T r a i n e r A i r c r a f t E x t r a c t e d from F l i g h t Data: M o d i f i e d Newton-Raphson Analys is . NADC-74181-30-VOL-1 AD-A013181. Naval A i r Development Center, Warminster, Pennsylvania, June 23, 1975.

Comparison f o r t h e E s t i m a t i o n of S t a b i l i t y D e r i v a t i v e s Cons ider ing Gust Dis turbances. Feb. 1975. ( E n g l i s h T r a n s l a t i o n : European Space Agency TT 258.)

Mess - und Systemrauschen. Regelungstechnik, H e f t 10, pp. 324-330, 1977.

i m geschlossenen Rege lk re is . Regelungstechnik und Prozess-Datenverarbeitung, v o l . 19, pp. 113-119, 1971.

A Comparison of I d e n t i f i c a t i o n Techniques; Volume I-Data A c q u i s i t i o n and

Schulz, G.: Maximum L i k e l i h o o d I d e n t i f i c a t i o n Using Kalman F i l t e r i n g Least-Squares Es t imat ion . A DLR-FB 75-94,

Schulz , G.: Entwur f o p t i m a l e r E ingangssignale filr d i e S y s t e m - i d e n t i f i z i e r u n g u n t e r Beruecks ich t igung von

Anwendung von Schaetzver fahren fur d i e Kenngrossen von Regels t recken aufgrund von Messungen Schulze, H . :

Schwalm, D.: Bestimnung des Frequenzganges eines l i n e a r e n rueckgekoppel ten Systems m i t zwei unabhaengi- gen s tochas t ischen Eingangssignalen. Regelungstechnik und Prozess-Datenverarbeitung, v o l . 18,

Schweppe, Fred C.: U n c e r t a i n Dynamic Systems. P r e n t i c e - H a l l , Englewood C l i f f s , New Jersey, 1973.

Shafer, Mary F.: S t a b i l i t y and Cont ro l D r i v a t i v e s o f t h e T-376 A i rp lane. NASA TM X-56036, Sept. 1975.

Shafer, Mary F.: F l igh t -Determined Cor rec t ion Terms f o r Angle o f A t tack and S i d e s l i p . A I A A

Shafer, Mary F.:

pp. 453-455, 1970.

Paper 82-1374, Aug. 1982 (a ) .

J. Guid. C o n t r o l Dynam., vol . 5, no. 5, pp. 504-511, Sept.-Oct. 1982 (b).

C o e f f i c i e n t s From Trans ien t Response Data. NACA TN-2341. Apr. 1951.

Space S h u t t l e O r b i t e r F l i g h t Pressure Data t o Determine A i r Data - STS 1-4. Jan. 1983.

Low-Order Equ iva len t Models o f H i g h l y Augmented A i r c r a f t Determined from F l i g h t Data.

S h i n b r o t , Marvin: A Least-Squares Curve F i t t i n g Method With A p p l i c a t i o n t o t h e C a l c u l a t i o n of S t a b i l i t y

Siemers, P.M., 111; Wolf, H.; and Flanagan, P.F.: S h u t t l e Ent ry A i r Data System Concepts App l ied t o A I A A Paper 83-0118,

Sim, Alex G.: A C o r r e l a t i o n Between F l igh t -Determined D e r i v a t i v e s and Wind-Tunnel Data f o r t h e X-246

S isk , T.R.: A Technique f o r t h e Assessment o f F i g h t e r A i r c r a f t P r e c i s i o n C o n t r o l l a b i l i t y . A I A A

Skudr idak is , Jean: Systemnodel l ierunq Und I d e n t i f i z i e rung von 'Squ iva len ten ' Systemen m i t und ohne

Research A i r c r a f t . NASA SX-3371, 1976.

Paper 78-1364, Aug. 1978.

E r s a t z t o t z e i t f e u r reglergesteutzte-Flugeuge. t i o n ESA-TT-852.)

DFVLR-FB 83-036, k v . 1983.. ( A l s o pub1 ished as t r a n s l a -

Smith, H.J.: F l igh t -Determined S t a b i l i t y and C o n t r o l D e r i v a t i v e s f o r an Execut ive J e t Transpor t . NASA

Smith, R . H . : A Theory f o r L o n g i t u d i n a l Shor t -Per iod P i l o t Induced O s c i l l a t i o n s . AFFDL-TR-77-57,

Smith, B.T.; Boyle, J.M.; Dongarra, J.J.; Garbow. B.S.; Ikebe, Y.; Klema, V.C.; and Moler, C.B.: M a t r i x

TM X-56034, J u l y 1975.

AD-A056982, June 1977.

Eigensystem Routines-EISPack Guide. Second ed. Spr inger -Ver lag , B e r l i n , 1976.

i n Closed Loop. I n t . J. Cont ro l , vo l . 21, no. 2, pp. 243-255, Feb. 1975.

Systems Opera t ing Under Feedback.

SBderstrBm. T,; Gustavsson, I.; and Ljung, L.:

S B d e r s t r h , T.; L jung, L.; and Gustavsson, I.:

Sorensen, John A.:

Sorenson, Haro ld W.: Parameter Es t imat ion ; P r i n c i p l e s and Problems. Marcel Dekker. Inc., New York,

I d e n t i f i a b i l i t y Cond i t ions f o r L i n e a r Systems Opera t ing

I d e n t i f i a b i l i t y Cond i t ions f o r L i n e a r M u l t i v a r i a b l e IEEE Trans. Automat. Cont ro l , vol . AC-21, pp. 837-840, Dec. 1976,

A n a l y s i s o f Ins t rumenta t ion E r r o r E f f e c t s on t h e I d e n t i f i c a t i o n Accuracy of A i r c r a f t Parameters. NASA CR-112121, 1972.

1980.

S t a l f o r d , H.L.: A p p l i c a t i o n o f t h e Es t imat ion-Before-Mode l l ing (EBM) System I d e n t i f i c a t i o n Method t o t h e H igh Angle o f A t t a c k / S i d e s l i p F l i g h t o f the T-2C Jet T r a i n e r A i r c r a f t . Dynamics Research Corpora t ion , System D i v i s i o n , Wi lmington, Massachusetts, Nov. 1979.

J. A i r c r a f t , v o l . 18, no. 10. pp. 801-809, Oct . 1981.

Three vols., AD-A079924.

S t a l f o r d , H.L.: High-Alpha Aerodynamic Model I d e n t i f i c a t i o n o f T-2C A i r c r a f t Using t h e EBM Method.

16

Steers, Sandra Thornberry; and I l i f f , Kenneth W.: E f f e c t s o f T ime-Sh i f t ed Data on F l i g h t - D e t e r m i n e d

Stepner , D.E.; and Mehra, R.K.: Maximum L i k e l i h o o d I d e n t i f i c a t i o n and Opt imal I n p u t Design f o r

S t a b i l i t y and C o n t r o l D e r i v a t i v e s . NASA TN D-7830, 1975.

I d e n t i f y i n g A i r c r a f t S t a b i l i t y and C o n t r o l D e r i v a t i v e s . NASA CR-2200, 1973.

Stewar t , G.W., 111: A M o d i f i c a t i o n o f Davidon 's M i n i m i z a t i o n Method t o Accept D i f f e r e n c e Approx ima t ion o f D e r i v a t i v e s . J. ACM, vo l . 14, no. 1, pp. 72-83, Jan. 1967.

St rang, G i l b e r t : L inea r A lgebra and I t s A p p l i c a t i o n s . Second ed. Academic Press, New York, 1980.

Subke, H.: Test I n s t a l l a t i o n s t o I n v e s t i g a t e t h e Dynamic Behaviour o f A i r c r a f t w i t h Scaled Models i n Symposium Dynamic Ana lys i s o f V e h i c l e R ide and Manoeuvering C h a r a c t e r i s t i c s , London, Wind Tunnels.

P r e p r i n t pp. 137-148, Nov. 28-30, 1978.

S u i t , W i l l i a m T.: D-6643, 1972.

Aerodynamic Parameters o f t h e Navion A i r p l a n e E x t r a c t e d f rom F l i g h t Data. NASA TN

Tanner, Russel R.; and Montgomery, Te r ry D.: S t a b i l i t y and C o n t r o l D e r i v a t i v e Es t ima tes Obta ined From F l i g h t Data f o r t h e Beech 99 A i r c r a f t . NASA TM-72863, 1979.

A p p l i c a t i o n i n A i r c r a f t F l i g h t Tes t i ng , NASA TN D-7647, pp. 291-313, 1974. T a y l o r , L.W., Jr.: A New C r i t e r i o n f o r Mode l i ng Systems. Parameter E s t i m a t i o n Techniques and

T a y l o r , L.W., Jr.: A p p l i c a t i o n o f a New C r i t e r i o n f o r M o d e l l i n g Systems. Methods f o r A i r c r a f t S t a t e and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 4, May 1974.

T a y l o r , Lawrence W., Jr.; and I l i f f , Kenneth W.: A M o d i f i e d Newton-Raphson Method f o r De te rm in ing S t a b i l i t y D e r i v a t i v e s f rom F l i g h t Data. Second I n t e r n a t i o n a l Conference on Computing Methods i n O p t i m i z a t i o n Problems, San Remo, I t a l y , Sept. 9-13, 1968, pp. 353-364, Academic Press, New York, 1969.

T a y l o r , Lawrence W., Jr.; and I l i f f , Kenneth W.: Systems I d e n t i f i c a t i o n Using a M o d i f i e d Newton-Raphson Method: A FORTRAN Program. NASA TN D-6734, 1972.

Thomas, H.H.B.M.; and Edwards, Gera ld ine : Mathemat ica l Models o f A i r c r a f t Dynamics f o r Extreme F l i g h t C o n d i t i o n s (Theory and Exper iment) . Dynamic S t a b i l i t y Parameters, AGARD-CP-235, Paper 27, Nov. 1978.

Thomas, H.H.B.M.; and Ross, A. Jean: The Ro le o f T h e o r e t i c a l S tud ies o f F l i g h t Dynamics i n R e l a t i o n t o F l i g h t Tes t i ng . S t a b i l i t y and C o n t r o l , AGARD-CP-119, Paper 22, Nov. 1972.

S t a b i l i t y and C o n t r o l D e r i v a t i v e s o f a T ranspor t H e l i c o p t e r . U n i v e r s i t y , Washington, D.C., Dec. 1976.

Tomaine, R.L.: The E f f e c t o f P i l o t C o n t r o l I n p u t Shape on t h e I d e n t i f i c a t i o n o f S i x Degree-of-Freedom M a s t e r ' s Thesis , George Washington

Tomaine. R.L.: F l i g h t Data I d e n t i f i c a t i o n o f S i x Degree-of-Freedom S t a b i l i t y and C o n t r o l D e r i v a t i v e s o f a Large "Crane" Type He l i cop te r . NASA TM X-73958, 1976.

European R o t o r c r a f t and Powered L i f t A i r c r a f t Forum, St resa, I t a l y , Paper 73, Sept. 13-15, 1978.

Models. Advances i n t h e Techniques and Technology o f t h e A p p l i c a t i o n o f Non l i nea r F i l t e r s and Kalman F i l t e r s , AGARD-AG-256, Paper 7, Mar. 1982.

Tomaine, R.L.; B ryan t , W.H.; and Hodge, W.F.: VALT Parameter I d e n t i f i c a t i o n F l i g h t Test . F o u r t h

T rank le , T.L.; V incent , J.H.; and F r a n k l i n , S.N.: System I d e n t i f i c a t i o n o f Non l i nea r Aerodynamic

T renk le , F.; and Reinhardt , M.: I n F l i g h t Temperature Measurements. AGARD-AG-160, vo l . 2, 1973.

Twisdale. T.R.; Jones, G.L.; and Ashurst , T.A.: A M i s s i o n O r i e n t e d F l i g h t Test Technique f o r I d e n t i f y i n g A i r c r a f t and F l i g h t Contro l System T r a n s f e r Funct ions. F l i g h t Test Techniques, AGARD-CP-223, Paper 13, Apr. 1977.

On t h e R e l a t i o n Between Weighted Least-Squares E s t i m a t o r s and I n s t r u m e n t a l V a r i a b l e Es t ima to rs . F o u r t h IFAC Symposium on I d e n t i f i c a t i o n and System Parameter E s t i m a t i o n , T b i l i s i , U.S.S.R., Sept. 21-27, 1976, Naum S. Raibman, ed., Nor th Hol land, Amsterdam and New York, 1978.

AGARD F l i g h t Tes t I ns t rumen ta t i on Ser ies , AGARD-AG-160, vo l . 8, 1977.

L a b o r a t o r y NLR-TR-76133-U, The Nether lands, May 1976.

1969.

Van den Boom, A.J.W.:

Van d e r Linen, J.C.; and Mensink, H.A.: L i n e a r and Angular P o s i t i o n Measurement o f A i r c r a f t Components.

Van d e r W i l t , M.: F l i g h t - P a t h Recons t ruc t i on o f Symmetric Unsteady F l i g h t s . N a t i o n a l Aerospace

Van Trees, H. L.: Detect ion, E s t i m a t i o n and Modu la t i on Theory. Volume 1. John Wi ley & Sons, New York,

Van Woerkom, K.: Symmetr ica l F l i g h t Condi t ions w i t h t h e Hawker Hunter Mk V I I . o f Aerospace Engineer ing, D e l f t , The Nether lands, Repor t LR-308, Jan. 1981.

Design and E v a l u a t i o n o f an I n s t r u m e n t a t i o n System f o r Measurements i n Nonsteady D e l f t U n i v e r s i t y o f Technology, Department

1 7

Vaughan, David R.:

V e l k o f f , H.R.: Technica l E v a l u a t i o n Report on t h e F l i g h t Mechanics Panel Symposium on R o t o r c r a f t Design.

Verbrugge, R.; R o t a t i v e Balance o f I.M.F. L i l l e and Assoc ia ted Exper imenta l Techniques. NASA TM-75886, 1981. ( T r a n s l a t i o n o f Balance r e o t a t i v e 'de-71 I.M.F. L i l l e e t Techniques Exper imenta les Associees ' . AAAF Paper NT 80-13, L i l l e , 1979.)

A Nonrecu rs i ve A lgeb ra i c S o l u t i o n f o r t h e D i s c r e t e R i c c a t i Equat ion. I E E E Trans. Automat. C o n t r o l , vol. AC-15, pp. 597-599, Oct. 1970.

AGARD-AG-114, Jan. 1978.

Verbrugge, R.A.; Charon, W.; and Marchand, M.: Wind Tunnel and F r e e - F l i g h t Model I d e n t i f i c a t i o n

V incen t , J.H.; Gupta, N.K.; and H a l l , W.E., Jr.: Recent R e s u l t s i n Parameter I d e n t i f i c a t i o n f o r High

Exper ience. Parameter I d e n t i f i c a t i o n , AGARO-LS-104, Paper 9, Nov. 1979.

Ang le -o f -A t tack S t a l l Regimes. A I A A Paper 79-1640, Aug. 1979.

V legher t , J.P.K.:

Von de r Decken, Jan; Schmidt, Eberhard; and Schulze, Bernd: On t h e Test Procedures o f t h e D e r i v a t i v e

Measuring Cl imb Performance o f a P r o p e l l o r Engined T ranspor t Aeroplane Us ing t h e A c c e l e r a t i o n Technique, AGARD Rep. 127, May 1957.

Balances Used i n West Germany. Dynamic S t a b i l i t y Parameters, AGARD-CP-235, Paper 6, 1978.

Vo rch i k , B.G.: P lan t I d e n t i f i c a t i o n i n a S tochas t i c Closed-Loop System. Automat ion and Remote C o n t r o l , vo l . 36, pp. 550-565, Sept. 1975.

Automat ion and Remote C o n t r o l , vo l . 34, pp. 1069-1081, Oec. 1, 1973.

R. & M. 3699 (RAE Tech. Rep. 70228). 1970.

Vo rch i k , B.G.; F e t i s o v , V.N.; and Ste inberg, Sh. E.: I d e n t i f i c a t i o n o f a Closed-Loop S t o c h a s t i c System.

W a t e r f a l l , A.P.: A Technique f o r t h e Automatic D i g i t a l A n a l y s i s o f F l i g h t Dynamic Response Data. A.R.C.

Weiner, Norbe r t : E x t r a p o l a t i o n , I n t e r p o l a t i o n , and Smoothing o f S t a t i o n a r y Time S e r i e s : W i th Engi - n e e r i n g A p p l i c a t i o n s . John Wi ley & Sons, New York, 1949.

Proc. A I A A T h i r d Atmospheric F l i g h t Mechanics Conference, June 1976, pp. 101-1137, A I A A , New York, 1976, We l l s , W.R.; and Ramachandran, S.: F l i g h t Test Design f o r E f f i c i e n t E x t r a c t i o n o f A i r c r a f t Parameters.

Wel ls tead, P.E.; and Edmunds, J.M.: Least-Squares I d e n t i f i c a t i o n o f Closed-Loop Systems. I n t . J. C o n t r o l , vo l . 21, no. 4, pp. 689-699, Apr. 1975.

Parameters, AGARO-CP-235, Paper 16, Nov. 1978. Whitmoyer, R.A.: Aerodynamic I n t e r a c t i o n s on t h e F i g h t e r CCV Test A i r c r a f t . Dynamic S t a b i l i t y

Wiberg. Donald M.: Schaum's O u t l i n e o f Theory and Probems o f S t a t e Space and L i n e a r Systems. McGraw-Hil l Book Co., New York, 1971.

Wiberg, O.M.; B e l l v i l l e , J.W.; Brovko, 0.; Maine, R.E.; and Ta i , T.C.: Model ing and Parameter I d e n t i f i c a t i o n o f t h e Human R e s p i r a t o r y System. I E E E Trans. Automat. C o n t r o l , v o l AC-24, pp. 716-720, Oct. 1979.

Wilhelm, K . ; and Verbrugge, R.A.: C o r r e l a t i o n Aspects i n t h e I d e n t i f i c a t i o n o f Dynamic E f f e c t s Us ing Complementary Techniques, F l i g h t i n Turbulence: Gust A l l e v i a t i o n . Ground F l i g h t Test Techniques and C o r r e l a t i o n , AGARD-CP-339, Paper 17, Feb. 1982.

W i l k inson , James H.: The A l g e b r a i c Eigenvalue Problem. Clarendon Press, Oxford, 1965.

W i l l i a m s , D.A.: The A n a l y s i s o f Random Data. AGARD-AG-160, vo l . 14, 1981.

W i l l i a m s , James L.; and S u i t , W i l l i a m T.: E x t r a c t i o n From F l i g h t Data o f L a t e r a l Aerodynamic C o e f f i c i e n t s f o r F-8 A i r c r a f t Wi th S u p e r c r i t i c a l Wing. NASA TN D-7749, 1974.

W i l l i a m s J.E.; and Vukel ich, S.R.: The USAF S t a b i l i t y and C o n t r o l D i g i t a l Datcom, Volume 1 U s e r ' s Manual. AFFDL-TR-79-3032, AD-A086557, Apr. 1979.

TR-75-32, A i r Force F l i g h t Test Center , Edwards A i r Fo rce Base, C a l i f o r n i a , Jan. 1976. Wilson, Donald B.; and Winters , Char les P.: F-15A Approach-to-Stall/Stall/Post-Stall Eva lua t i on . AFFTC

Wingrove, R.C.: A p p l i c a t i o n s o f a Technique f o r E s t i m a t i n g A i r c r a f t S t a t e s f rom Recorded F l i g h t Tes t Data. A I A A Paper 72-965, Sept. 1972.

c r a f t , vo l . 10, no. 5, pp. 303-307, May 1973. Wingrove, R.C.: Q u a s i - L i n e a r i z a t i o n Technique f o r E s t i m a t i n g A i r c r a f t S t a t e s f rom F l i g h t Data. J. A i r -

Wingrove, R,C.: Parameter F z t i m g t i n r ! of Powered-Lift S?QL ! , i r c ra f t Ch;r;cteri;tiCS :i i i: i iding i u i h i i r i i c e and Ground E f f e c t s . Methods f o r A i r c r a f t S ta te and Parameter I d e n t i f i c a t i o n , AGARD-CP-172, Paper 28, May 1975.

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Wolowicz, Chester H.: Considerat ions i n t h e De te rm ina t ion of S t a b i l i t y and C o n t r o l D e r i v a t i v e s and Dynamic C h a r a c t e r i s t i c s f rom F l i g h t Data. AGARD-AR-549, Pa r t 1, 1966.

Wolowicz, Chester H.; and Holleman, E u c l i d C.: S t a b i l i t y - D e r i v a t i v e De te rm ina t ion f rom F l i g h t Data. AGARD Rep. 224, Oct. 1958.

Wolowicz, Chester H.; and Yancy, Roxanah 6.: Exper imenta l De te rm ina t ion o f A i r p l a n e Mass and I n e r t i a l C h a r a c t e r i s t i c s . NASA TR R-433, 1974.

Wong, K.V.; and Polak, E.: I d e n t i f i c a t i o n o f L i n e a r D i s c r e t e Time Systems Us ing t h e I n s t r u m e n t a l V a r i a b l e Method. I E E E Trans. Automat. Con t ro l , v o l . AC-12, no. 6 , pp. 707-718, Dec. 1967.

Wuest, W.: Pressure and Flow Measurement - F l i g h t Tes t i ng . AGARD-AG-160, v o l . 11, 1980.

Yazawa, K e n j i : I d e n t i f i c a t i o n o f A i r c r a f t S t a b i l i t y and C o n t r o l D e r i v a t i v e s i n t h e Presence o f Turbulence. A I A A Paper 77-1134, Aug. 1977.

Yosida, Kosaku: Func t i ona l Ana lys i s . Second ed. Sp r inge r -Ver lag . B e r l i n , 1968.

Zacks, Shelemyahu: The Theory o f S t a t i s t i c a l I n fe rence . John Wi ley & Sons, New York, 1971.

Zadeh, L o t f i A.: and Desoer, Char les A.: L i n e a r System Theory. HcGraw-Hi l l Book Co., New York, 1963.

Zverev, A. I . : Handbook o f F i l t e r Synthes is . Wi ley, New York, 1967.

1. Report No.

NASA TM-86804

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7. Author(s) Kenneth W. I l i f f and R i c h a r d E. Maine

2. Government Accession No. 3. Recipient's Catalog No.

8. Performing Organization Report No. H-1358

4. Title and Subtitle

B i b 1 i o g r a p h y f o r A i r c r a f t Parameter E s t i m a t i o n 5. Report Date

6. Performing Organization Code

October 1986

T h i s document i s t h e r e s u l t o f an e f f o r t t o c o m p i l e an e x t e n s i v e b i b l i o g r a p h y i n t h e f i e l d o f a i r c r a f t pa ramete r e s t i m a t i o n . T h i s l i s t c o n t a i n s d e f i n i t i v e works r e l a t e d t o most a i r c r a f t parameter e s t i m a t i o n approaches. T h e o r e t i c a l s t u d i e s as w e l l as p r a c t i c a l a p p l i c a t i o n s a r e i n c l u d e d . Many o f t h e s e p u b l i c a t i o n s a r e p e r t i n e n t t o s u b j e c t s p e r i p h - e r a l l y r e l a t e d t o parameter e s t i m a t i o n , such a s a i r c r a f t maneuver d e s i g n o r i n s t r u m e n t a t i o n c o n s i d e r a t i o n s .

9. Performing Organization Name and Address NASA Ames Research Cen te r Dryden F1 i g h t Research F a c i l i t y P.O. Box 273 Edwards, CA 93523-5000

12. Sponsoring Agency Name and Address

N a t i o n a l A e r o n a u t i c s and Space A d m i n i s t r a t i o n Washington, D.C. 20546

17. Key Words (Suggested by Authorb))

A i r c r a f t f l i g h t t e s t i n g A i r c r a f t s t a b i l i t y and c o n t r o l B i b l i o g r a p h y Maximum 1 i k e l i hood Pa ramet e r e s t i mat i on

10. Work Unit No.

RTOP 505-61

11. Contract or Grant No.

13. Type of Report and Period Covered

Tec hn i c a l Memorandum

14. Sponsoring Agency Code

18. Distribution Statement

U n c l a s s i f i e d - U n l i m i t e d

~~

19. Security Classif. (of this report) 20. Security Classif. (of this page) 21. No. of Pages

U n c l a s s i f i e d Unc 1 ass i f i ed 21

STAR c a t e g o r y 05

22. Price"

A02