Brigham Young University BYU ScholarsArchive All Faculty Publications 1999-8 Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation Timothy McLain Mechanical Engineering Department, Brigham Young University, [email protected] Randal W. Beard Department of Electrical and Computer Engineering, Brigham Young University, [email protected] Follow this and additional works at: hps://scholarsarchive.byu.edu/facpub Part of the Mechanical Engineering Commons Original Publication Citation McLain, T. and Beard, R. Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation, Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA-1999-3997, August 1999, Portland, Oregon. is Conference Paper is brought to you for free and open access by BYU ScholarsArchive. It has been accepted for inclusion in All Faculty Publications by an authorized administrator of BYU ScholarsArchive. For more information, please contact [email protected], [email protected]. BYU ScholarsArchive Citation McLain, Timothy and Beard, Randal W., "Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation" (1999). All Faculty Publications. 1935. hps://scholarsarchive.byu.edu/facpub/1935
Welcome message from author
This document is posted to help you gain knowledge. Please leave a comment to let me know what you think about it! Share it to your friends and learn new things together.
Transcript
Brigham Young UniversityBYU ScholarsArchive
All Faculty Publications
1999-8
Nonlinear Robust Missile Autopilot Design UsingSuccessive Galerkin ApproximationTimothy McLainMechanical Engineering Department, Brigham Young University, [email protected]
Randal W. BeardDepartment of Electrical and Computer Engineering, Brigham Young University, [email protected]
Follow this and additional works at: https://scholarsarchive.byu.edu/facpubPart of the Mechanical Engineering Commons
Original Publication CitationMcLain, T. and Beard, R. Nonlinear Robust Missile Autopilot Design Using Successive GalerkinApproximation, Proceedings of the AIAA Guidance, Navigation, and Control Conference,AIAA-1999-3997, August 1999, Portland, Oregon.
This Conference Paper is brought to you for free and open access by BYU ScholarsArchive. It has been accepted for inclusion in All Faculty Publicationsby an authorized administrator of BYU ScholarsArchive. For more information, please contact [email protected], [email protected].
BYU ScholarsArchive CitationMcLain, Timothy and Beard, Randal W., "Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation"(1999). All Faculty Publications. 1935.https://scholarsarchive.byu.edu/facpub/1935
Fz
My
V
α
δ
z
0 0.2 0.4 0.6 0.8 1−50
0
50
100
150Pitch Rate
time (s)
q (d
eg/s
)
0 0.2 0.4 0.6 0.8 10
5
10
15
20Angle of Attack
time (s)
α (d
eg)
µ=0, ν=0µ=3, ν=3µ=.25, ν=.25µ=.25, ν=3µ=3, ν=.25
0 0.2 0.4 0.6 0.8 1−600
−400
−200
0
200
400Fin Deflection Rate
time (s)
dδ/d
t (de
g/s)
0 0.2 0.4 0.6 0.8 1−20
−15
−10
−5
0
5Fin Deflection
time (s)
δ (d
eg)
0 0.2 0.4 0.6 0.8 10
20
40
60
80
100
120
140Pitch Rate
time (s)
q (d
eg/s
)
0 0.2 0.4 0.6 0.8 10
5
10
15
20Angle of Attack
time (s)
α (d
eg)
0 0.2 0.4 0.6 0.8 1−20
−15
−10
−5
0
5Fin Deflection
time (s)
δ (d
eg)
0 0.2 0.4 0.6 0.8 1−0.4
−0.2
0
0.2
0.4
0.6Worst−case Parameter Variations
time (s)
µ &
ν
µν
Related Documents
![Robust H Autopilot Design for Agile Missile With …batti/progetti_fda/47.pdfII. MISSILE MODELING A. Nonlinear Model In this paper, the AIM-9X missile [18] equipped with a thrust vectoring](https://static.cupdf.com/doc/110x72/5e8e2fd0378fff744940f04c/robust-h-autopilot-design-for-agile-missile-with-battiprogettifda47pdf-ii-missile.jpg)
