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NUMERO DOCUMENT/DOCUMENT NUMBER FORMAT/SIZE PAGE

62 262 801 - 090 A4 1/66

THALES AIR SYSTEMSF8224 REV B

Ce document et les informations quil contient sont confidentiels et sont la propritexclusive de THALES. Ils ne doivent tre communiqus quaux personnes ayant enconnatre et ne peuvent tre reproduits ni divulgus toute autre personne sanslautorisation pralable crite de THALES AIR SYSTEMS SA.

This document and the information it contains are property of THALES AIR DEFENCE andconfidential. They shall not be reproduced nor disclosed to any person except to thosehaving a need to know them, without prior written consent of THALES AIR SYSTEMS SA

CAHIER DE PROCEDUREDACCEPTATION

ACCEPTANCE TEST PROCEDURE

STAR 2000 - RSM970S CIRIUS

N62 262 801

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THALES Air Systems F8224 62 262 801 - 090 Rev. B A4 3/66

Ce document et les informations quil contient sont confidentiels et sont la propritexclusive de THALES. Ils ne doivent tre communiqus quaux personnes ayant enconnatre et ne peuvent tre reproduits ni divulgus toute autre personne sanslautorisation pralable crite de THALES AIR SYSTEMS S.A.

This document and the information it contains are property of THALES and confidential.They shall not be reproduced nor disclosed to any person except to those having a need toknow them, without prior written consent of THALES AIR SYSTEMS S.A.

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SOMMAIREContents

1. OBJETPurpose

2. DOCUMENTS APPLICABLESApplied documents

3. COMPOSITION DE LA FOURNITUREEquipment breakdown

4. MESURES ET TESTSMeasurements and tests

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1. OBJET:Purpose

Ce document a pour but de normaliser lacceptation site technique de la fourniture suivante.This document defines the technical site acceptance of the following supply:

STAR 2000 and RSM970S CIRIUS

2. DOCUMENTS APPLICABLES:Applied documents

Title Rfrence Code Indice

Cahier de rsultats dessaisSAT Technique

SAT Tests Report Book

62 262 801

62 262 801

088

088

Dernier indice

Last revision

3. COMPOSITION DE LA FOURNITURE:Equipment breakdown

La composition de la fourniture est donne en annexe 1 du Cahier de Rsultats dEssais.See equipment breakdown in appendix 1 of Acceptance Tests Report book.

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4. MEASUREMENTS AND TESTS

4.1. LIST OF TEST EQUIPMENT

See list of test equipment in SAT Tests Report book.

4.2. LIST OF MEASUREMENTS AND TESTS

4.2.1. RADAR STATION

Concerned Proceduresheet

Nr

Title

Softwares

Antenna tilts

Parameters

1G

2G

3G

Software versions

Tilt reference

Recording parameters

4.2.2. PRIMARY RADAR

Concerned equipment Proceduresheet

Nr

Title

RF LINKS

POWER SUPPLYCABINET AE 2000

AA 2000, EA2000 andAN2000

ANTENNA ENCODING

TRANSMITTER SST2000

GENERATOR RECEIVERGRA 2500S

RADAR ELECTRONICS

RADAR ELECTRONICS

RADAR ELECTRONICS

RADAR ELECTRONICS

DISPLAY UNIT IBIS

COMPRESSOR

1P

2P

3P

4P

5P

6P

7P

8P

9P

10P

11P

12P

VSWR and Losses

Distribution, safeties

Aerial control and safeties

Antenna encoding

Transmitted signal power

Noise level

Phase Stability

A channel / B channel switching

Coverage switching display

STC laws Display

Digital and synthetic videos

Pressure level

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4.2.3. SECONDARY RADAR


Nr

Title

RF LINKS

RADAR ELECTRONICS

SSR TRANSMITTER

MODE S TRANSMITTER

TRANSMITTER

TRANSMITTER

RECEIVER

RECEIVER

RADAR ELECTRONICS

RECEIVER

RADAR ELECTRONICS

RADAR ELECTRONICS

RADAR ELECTRONICS

RADAR ELECTRONICS

RADAR ELECTRONICS

RADAR ELECTRONICS

RADAR ELECTRONICS

1S

2S

3S

4S

5S

6S

7S

8S

9S

10S

11S

12S

13S

14S

15S

16S

17S

VSWR and Losses

Trigger and staggering

Pulse width

Pulse width

Transmitted signal power

IISLS function

Receiver sensitivity

Receiver bandwidth

TVBC laws

RSLS function

Internal test plot

Site Monitor

BDS Extraction

Off line test

Automatic or manual switching

Encoder failure

Time stamping (option)

4.2.4. REMOTE CONTROL AND MONITORING SYSTEM


Nr

Title

RCMS 1.1R

1.2R

1.3R

Remote Control and Monitoring System

RCMS Daily log

STM/LTM control

4.2.5. RADAR SYSTEM


Nr

Title

Endurance test 1RS 72h Endurance Test

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MEASUREMENT PROCEDURE SHEET Nr. 1G 1/1

1. EQUIPMENT OR MAIN ELEMENT INVOLVED: SOFTWARES

2. TESTED FUNCTION: SOFTWARES VERSIONS

3. PURPOSE: Record the reference software of the station

4. RECOMMENDED TEST TOOLS: None

5. INSTRUCTIONS:

Open a command prompt window on LTM (Local Terminal Monitor) or on IBIS.

Type telnet 192.1.1.32(TMR channel A) or 192.1.1.36(TMR channel B)Login: tmr

(1) Note the reference software of the current version for each channel.

Type exit

(2) Perform the same procedure with the address 192.1.1.80(DPC channel 1) and 192.1.1.84(DPC channel 2)and the login irp.

(3-4) On the CBP TMR STAR, in the menu help/About CBPnote the values of the version number and the ParamConfig version number.

(5-6) On the CBP RSM970S CIRIUS, in the menu help/About CBPnote the values of the version number and theParam Config version number.

(7) On the IBIS, in the menu About / information, note the soft revision.

(8) On the RCMS, in the menu help / about RCMSnote the RCMS version

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THALES Air Defence F8224 62 262 801 - 090 Rev. - A4 8/65

Ce document et les informations quil contient sont confidentiels et sont la propritexclusive de THALES. Ils ne doivent tre communiqus quaux personnes ayant enconnatre et ne peuvent tre reproduits ni divulgus toute autre personne sanslautorisation pralable crite de THALES AIR DEFENCE S.A.

This document and the information it contains are property of THALES and confidential.They shall not be reproduced nor disclosed to any person except to those having a need toknow them, without prior written consent of THALES AIR DEFENCE S.A.

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: ANTENNA TILTS

2. TESTED FUNCTION: TILT REFERENCE

3. PURPOSE: Evaluation of the coverage


5. INSTRUCTIONS:

(9-10) Read the value directly on the Primary and secondary antenna cursors.

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: PARAMETERS

2. TESTED FUNCTION: RECORDING PARAMETERS

3. PURPOSE: Record the operational parameters


5. INSTRUCTIONS:

Primary parameters recording:

- With the CBP TMR STAR, in the menu command/Transfertfrom radarselect current parametersand Allparameters, save the parameter file (*.tmr) in a directory.

- With the CBP TMR STAR, in the menu command/Transfertfrom radarselect configuration parametersand Allparameterssave the configuration files (*.dfa,*.pca,*.dfw,*.pcw,*.thw,*.cdw) in the previous directory.

(11-12) Note the name of this directory and the date on the CRE.

- Perform this recording on the other channel with an other directory

- With the CBP RSM970S CIRIUS, in the menu command/Transfertfrom radarselect current parameterssave theparameter files (*.gbl,*.cmp,*.rps,*.cov) in a directory.

(13-14) Note the name of this directory and the date on the CRE.

- Perform this recording on the other channel with an other directory

- Make two official copy (one for the customer, one for THALES)

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MEASUREMENT PROCEDURE SHEET Nr. 1P 1/2

1. EQUIPMENT OR MAIN ELEMENT INVOLVED: PRIMARY RF LINKS

2. TESTED FUNCTION: VSWR AND LOSSES

3. PURPOSE: Measure the VSWR and LOSSES due to RF cables and waveguide

4. RECOMMENDED TEST TOOLS:

STANDARD TOOL: SWR/LOSSES METER WILTRON S331 or Equivalent1 S band transition wave guide- coax

5. INSTRUCTIONS:

TEST TO BE PERFORMED ONLY DURING THE INSTALLATION PERIOD

All VSWR measurement should be performed in rotationSWITCH OFF THE TRANSMITTER.

5.1 VSWR MEASUREMENT

5.1.1 Wave guide (aircraft low beam)

Perform the following instructions

Above the microwave assembly, separate the wave guide from the microwave assembly output, and fix a transitionon the aerial wave guide

Connect the TEST EQUIPMENT output on the waveguide transition

Calibration

Set the polarization on circular

Switch on the SITE MASTER, program the start frequency to 2700 Mhz and the stop frequency to 2900 MHz.

Connect the test cable to the PORT TEST of the SITE MASTER and perform CALIBRATION following instructionson the screen.

Select the markers on F1 and F2 and choose the automatic scale.

Measurement

Connect the test cable to the waveguide transition.(15-16) Select the SWR mode and perform a continuous measurement for the two frequencies.

Save the measurement and transfer it on a PC to be printed.(17-18) Repeat the measurements on linear polarization.

5.1.2 Coaxial cables (aircraft high beam and both weather beams )

The measurement should be performed on both circular and linear polarization

On Microwave Assembly, disconnect the coaxial cable of the tested channel and connect the SITE MASTER to thiscable.

(19 to 30) Repeat the previous procedure for aircraft high beam and weather beams (options)

Specification

VSWR 1.5

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5.2 LOSSES MEASUREMENT

Switch the transmitter and the antenna rotation off.

5.2.1 Wave guide (aircraft low beam)

Calibration

Switch on the SITE MASTER, program the start frequency to 2700 Mhz and the stop frequency to 2900 MHz


Select the markers on F1 and F2 and choose the automatic scale.

Measurement

Connect the test cable to the waveguide transition.

Open the waveguide line above the rotating joint and close the waveguide by a flat metallic plate.(31-32) Select the CABLE LOSS mode and perform a continuous measurement for the two frequencies.

Save the measurement and transfer it on a PC to be printed.

Specification

Aircraft LB for F1 and F2 (wave guide) ( 0.5dB + 0.016 dB /m ) + 10%

5.2.2 Coaxial cables (aircraft high beam and both weather beams)

Measurement

Connect the SITE MASTER to the tested channel cable Disconnect the antenna cables from the output of the rotating joint (upper part) corresponding to the channel and

replace it by a SHORT transition.(33 to 38) Repeat the previous procedure for aircraft high beam and weather beams (option)

Specification

Aircraft HB for F1 and F2 ( 2.3dB + 0.068 dB /m ) + 10%

Weather LB for F1 and F2 (Option) ( 2.2dB + 0.068 dB /m ) + 10%

Weather HB for F1 and F2 (Option) ( 2.2dB + 0.068 dB /m ) + 10%

6. PUTTING IN NORMAL CONDITION:

Set the waveguides and cables at their initial state.

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: POWER SUPPLY CABINET AE 2000

2. TESTED FUNCTION: DISTRIBUTION, SAFETIES

3. PURPOSE: Check the power supply cabinet, safeties


5. INSTRUCTIONS:

Local power control:

Put the AE2000 cabinet in Local mode Switch off the TMR-PC (both channel), IBIS, LTM and DPC-PC (both channel) to avoid any power supply failure due

to the emergency stop

Push the emergency stop and check the general switching off.(39) Release the emergency stop and check that the switching on is performed after pushing the ON switch.

- The radar station is available for operation after a 5 minutes delay max.- The radar station is configured as before the shutdown of the station.

RCMS power control (remote):

Switch off the TMR-PC (both channel), IBIS and DPC-PC (both channel) to avoid any power supply failure due tothe emergency stop

Put the AE2000 cabinet in Remote mode

On RCMS, select ANCILLARIES box

Select POWER DISTRIBUTION box

Select Radar Control

Switch off the AE2000 cabinet from the RCMS LTM or STM.

Check that the radar switch off except the RCMS LTM, the WAGO, the RCMS modem (Optional) and the LocalDisplay.

(40) Switch on with the RCMS LTM or STM and check the return of the power on all radar equipment

- The radar station is available for operation after a 5 minutes delay max.- The radar station is configured as before the shutdown of the station.

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: AA2000, EA2000 and AN2000

2. TESTED FUNCTION: AERIAL CONTROL AND SAFETIES

3. PURPOSE: Check the aerial safeties.


5. INSTRUCTIONS:

5.1 Antenna Speed rotation

On the CBP RSM 970S CIRIUS of the master channel:

Select the menu Main measurements/Antenna rotation period per scan

(41) Note the display measurement.

5.2 Antenna Turntable

(42) Check the siren is working before antenna rotation.

(43-44) Check the antenna can be run by a dual motors or a single motor drive:Stop antenna rotation and restart successively with motor 1 and motor 2.

(45) Check good operation of a motor overheat switch of each drive motor on antenna control cabinet.

For AA2000-NGB

To simulate a motor overheat, disconnect successively on antenna control cabinet the points TB 2.17 (motor 1) andTB 2.19 (motor 2). Each time, observe stop of motor.

For AA2000-A (Automaton)To simulate a motor overheat, disconnect successively on antenna control cabinet the points TB 3.18 (motor 1) andTB 3.20 (motor 2). Each time, observe stop of motor.

(46) Check brake to prevent the aerial from rotating during maintenance.After stop antenna rotation, activate the brake and observe that the start of antenna rotation is not possible.

(47) When the emergency breaker of the antenna platform is pushed, check that the rotation is stopped.

(48) Check rotation is prevented when antenna door access is open.

For AA2000-A (Automaton), you must disconnect the safety key from the front panel to open the access door.

(49) Verify there are no oil leaks.

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: ANTENNA ENCODING

2. TESTED FUNCTION: ANTENNA ENCODING

3. PURPOSE: Check the presence of azimuth reference pulses (ARP) and azimuth clock pulses (ACP), and the voltageof encoder power supply.


STANDARD TOOL:

- Scope- Multimeter

5. INSTRUCTIONS:

5.1. Azimuth Reference Pulses and Azimuth Clock Pulses distribution.

(50) Check the presence of ARP and ACP by inserting a flat cable on connector P35 located on rear TMR panel

P35: ACP+: pin 1 ARP+: pin 3 ACP+: pin 7 ARP+: pin 9ACP-: pin 2 ARP- : pin 4 ACP- : pin 8 ARP-: pin 10

Perform the same measurements for both channels.

5.2. ARP Alignment

Connect the Oscilloscope on pin 3 and pin 9 of P35 connector of same TMR (A or B)(51) Check that time difference between both ARP is less than one ACP.

5.3. Power supply.

(52) In the TOM cabinet, measure the voltage +5V and +15V on both encoder power supply.

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: TRANSMITTER SST 2000

2. TESTED FUNCTION: TRANSMITTED SIGNAL POWER

3. PURPOSE: Check nominal power.


STANDARD TOOL: Peak power meter 8900C or Equivalent

5. INSTRUCTIONS:

On the Microwave assembly, disconnect output of DC5 coupler (N plug)(DC5 is the 1st coupler after transmitter output).

Connect the peak power meter to this output.

Switch thumb wheel RC1 of GRA interface board (TFH 343) to 4 (F1 frequency) and switch on the transmission.(53) Measure the signal peak power (Pc).

The transmitted peak power Pe = Pc + Att(Att = DC5 coupler attenuation + Attenuator 10dB)

(54) Perform again the measurement with GRA interface board (TFH 343) RC1 thumb wheel GRAswitched to 5 (F2 frequency).

(55) Stop antenna rotation, check the safety chain led is on (front board TGE 233 (primarytransmitter SST2000) and the transmission is off.

Repeat the test on Channel B


Put back the equipment in normal configuration. The interface board thumb wheel has to be switched to 0.

TRANSMITTER

Peak power meter

WAVEGUIDE

MICROWAVEASSEMBLY

DC5

Attenuator10dB

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: GENERATOR RECEIVER GRA2500S

2. TESTED FUNCTION: NOISE LEVEL

3. PURPOSE: Check the Noise Level at receiver output


5. INSTRUCTIONS:

On the CBP TMR STAR (Online channel)

Select the menu system measurements(56) Read the aircraft channel noise stddeviation on I & Qon the Master channel

If you have a weather channel option, select circular polarisation on the antenna cabinet(57) Read the weather channel noise stddeviation on I & Qon the Master channel

Switch the channel, wait 2 minutes and perform the same measurements on the other TMR.

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: RADAR ELECTRONICS

2. TESTED FUNCTION: PHASE STABILITY

3. PURPOSE: Measure the phase stability of the output transmitter RF signal.


5. INSTRUCTIONS:

On the SST2000, switch on the transmission.

On the CBP TMR STAR: (Online channel)

Select the menu System measurements

(58) Read the Stability measurement for f1 on the Master channel(59) Read the Stability measurement for f2on the Master channel

Switch the channel, wait 2 minutes and perform the same measurements on the other TMR.

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2. TESTED FUNCTION: A CHANNEL / B CHANNEL SWITCHING

3. PURPOSE: Check Channels switching


5. INSTRUCTIONS:

With the CBP TMR STAR, program the following parameter on each channel :

Menu DPC plot OutputDPC output characteristics

Test target is transmitted: true

With the CBP TMR STAR, program the following parameter on channel A :

Menu Test target controlOperational moving echo azimuth

value: 90

With the CBP TMR STAR, program the following parameter on channel B :

Menu Test target controlOperational moving echo azimuth

value: 180

Put all TMR and DPC in operational operating states.

With the CBP RSM970S CIRIUS, program the following parameter on both channels

Menu LD outputLD output selection

Plots output: true

(60) Check that the test plot is display in accordance with the master channel :Channel A master: test plot at 90Channel B master: test plot at 180

Disconnect the plug J22 behind the GRA of the master channel.

(61) Check that the test plot is display in accordance with the new master channel :Channel A master: test plot at 90Channel B master: test plot at 180

Repeat the test on the other channel.

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2. TESTED FUNCTION: COVERAGE SWITCHING DISPLAY

3. PURPOSE: Check the display of coverage switching.


5. INSTRUCTIONS:

5.1 Checking AIRCRAFT coverage switching:

With the CBP TMR STAR, program the following parameters :

Menu LD videoMaintenance video selection

Video selection: Aircraft HB LB map

Menu HB/LB Command ParametersAircraft HB LB map

Number of programmed azimuthal sectors: 4Map

Azimuthal sector (1)Start azimuth: 0Switch range: 6 Nm




Aircraft HB LB setting areasData

Aircraft HB LB area (0)

Area is used: trueStart range: 5 NmStop range: 6 NmStart azimuth: 270Stop azimuth: 359.89

Aircraft HB LB setting areas

Aircraft HB LB area [1] to [15]Area is used: false

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On the IBIS:

Open the layer dialog windows and select (if necessary) the raw video

On the left of the display, in the menu video, select the TMR maintenance video according to the channel online

(62) Check the display is identical with this diagram:

Repeat the test on Channel B

2 Nm

6 Nm

4 Nm

8 Nm

5 Nm

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5.2 Checking WEATHER coverage switching (OPTION):

On the AA2000:

Set the polarization switch to Circular position.



Video selection: Weather HB LB map

Menu HB/LB Command ParametersWeather HB LB map






On the IBIS:

Video settings are the same



Remove all sectors.

2 Nm

6 Nm

4 Nm

8 Nm

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2. TESTED FUNCTION: STC laws display

3. PURPOSE: Check the display of STC.


5. INSTRUCTIONS:

5.1 Checking Aircraft STC laws parameters:



Video selection: Aircraft STC map




Azimuthal sector (2)

Start azimuth: 180Switch range: 8 Nm

Aircraft HB LB setting areasAircraft HB LB area [0] to [15]

Area is used: false

Menu STC Command ParametersAircraft low beam LR STC law

Max value: 0dB

Aircraft low beam STC lawExponent: 1

Max range: 7.998NmMax value: 60dB

Aircraft high beam STC lawExponent: 3Max range: 7.998NmMax value: 60dB

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On the IBIS:

Video settings are the same as former test(64) Check the display is identical with this diagram:

(Picture not contractual: depends of the sequencing)

5.2 Checking Weather STC laws parameters (OPTION):

With the CBP TMR STAR, program the following parameters:


Video selection: Weather STC map

Menu HB/LB Command ParametersWeather HB LB map





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Menu STC Command ParametersWeather low beam STC law

Exponent: 1Max range: 7.998NmMax value: 60dB

Weather high beam STC law

Exponent: 3Max range: 7.998NmMax value: 60dB

On the IBIS:


(Picture not contractual: depends of the sequencing)

5. 3 Checking Aircraft STC cell:



Video selection: Aircraft STC map





Aircraft HB LB setting areasAircraft HB LB area [0] to [15]

Area is used: false

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: DISPLAY UNIT IBIS

2. TESTED FUNCTION: Digital and synthetic videos

3. PURPOSE: Checks of users function Selection and display of Digital Video signals


5. INSTRUCTIONS:

Check the availability of the following functions:

5.1.CHECKS OF USERS FUNCTIONS

(67) Check the availability of the following functions.

- Choice of scale- Filter Primary Tracks and Primary Plots

Choice of informations for the plots labels

Off-center of plots (plot offset) and choice of past positions (history)

Switch On/Off TMR-A and TMR-B , Checks of statistics on the sensors

General control :

- In the menu video: checks the afterglow of used videos.

On the Preferences window / Radar Image:Check the function by changing the range marker space, the azimuth markers space (number

of spokes) and the colour of the background.

- On the Preferences window / Sensor: change the colour for each sensor.

- On the plots menu, click on the plot selection mode button. In the selected plot windows, clickon the selected area button , define an area and check the information about the inside plots.

5.2. RAW VIDEO DISPLAY

(68) Check the primary raw videos display on IBIS (maintenance and operationnal).

5.3. SYNTHETIC DISPLAY

(69) Check the presence of the plots and tracks information for each channel.

(70) Check the presence of PSR plots and tracks information.

These tests are performed on opportunity traffic.

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: COMPRESSOR

2. FUNCTION TESTED: PRESSURE LEVEL

3. PURPOSE: Check level safeties and pressure level in the wave guide


5. INSTRUCTIONS:

5.1 PRESSURE ALARM LEVEL:

Remove slowly the air pipe from the compressor.

(71) Check the alarm threshold is less than 10 hpa

5.2 OPERATING FACTOR:

(72) Note the date and time of the day and the value of the counter (T1) at the front of the air dryer. This valuedescribe the working time of the compressor.

Wait at least 24h and notethe date and time of the day and the value of the counter (T2) at the front of theair dryer.

Calculate the elapse time between the two reading and the duration of working time T=T2-T1.

Calculate the ratio T / elapse time, the ratio should be less than 50%

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MEASUREMENT PROCEDURE SHEET Nr. 1S 1/1

1. EQUIPMENT OR MAIN ELEMENT INVOLVED: SECONDARY RF LINKS

2. TESTED FUNCTION: VSWR AND LOSSES

3. PURPOSE: Measure the VSWR and LOSSES due to RF cables


STANDARD TOOL: SWR/LOSSES METER WILTRON S331 or equivalent

5. INSTRUCTIONS:

All measurement should be performed in rotation with transmitter switch off.

5.1 VSWR MEASUREMENT

Perform the following instructions

Switch on the SITE MASTER, program the start frequency to 1000MHz and the stop frequency to 1100MHz.


Select the markers on 1030Mhz and 1090Mhz and choose the automatic scale.

Measurement

Connect the test cable to the coaxial cable of the channel.(100-101) Select the SWR mode and perform a continuous measurement.

Save the measurement and transfer it on a PC to be printed.

( 102 to 105) repeat the measurements on and channel .

Specification

VSWR 1.5

5.2 LOSSES MEASUREMENT

Switch on the SITE MASTER, program the start frequency to 1000 MHz and the stop frequency to 1100 MHz


Select the markers on 1030 Mhz and 1090 Mhz and choose the automatic scale.

Measurement

Connect the test cable to the coaxial cable of the channel. Disconnect the antenna cables from the output of the rotating joint (upper part) corresponding to the channel and

replace it by a SHORT transition.(106-107) Select the CABLE LOSS mode and perform a continuous measurement. Save the measurement and transfer it on a PC to be printed.

(108 to 111) Repeat the measurements on and channel.

Specification

Losses for, and (1030 Mhz and 1090 Mhz) ( 1.5dB + 0.025 dB /m ) + 10%


Set the waveguides and cables at their initial state.

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2. TESTED FUNCTION: TRIGGER AND STAGGERING

3. PURPOSE: Control the scheduling - Check the staggering steps


STANDARD TOOL: Oscilloscope or counter

5. INSTRUCTIONS:

Connect the scope on J410 of MDRP output.

5.1 CBP REFERENCE PARAMETERS

Read inside the CBP RSM970S CIRIUS parameters.

- On the Scheduling parameters / Operational pattern parameter

(112) Read the computed IRF(113) Read the RC duration(114) Read the AC duration

-For Mode SSR- Check on the scope or counter that the value is equal at the AC duration.- Check that the computed IRF = 1/(AC duration).

-For Mode S- Check on the scope or counter that the value is equal at the RC + AC duration.- Check that the computed IRF = 1/(RC+AC duration).

5.2 INTERNAL TRIGGER (number of period = 1)

- Set the staggering OFF with the CBP RSM970S CIRIUS.

- Scheduling parameters- ALL_CAL_STAGGERING_ENABLED = FALSE

- Check on the scope the effect.

- Set the staggering ON with the CBP RSM970S CIRIUS.

- Scheduling parameters- ALL_CAL_STAGGERING_ENABLED = TRUE

- Check on the scope the effect

(115) Note the result

Repeat the test on channel 2

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: SSR TRANSMITTER

2. TESTED FUNCTION: PULSES WIDTH, SSR

3. PURPOSE: Check the SSR width of transmitted pulses


STANDARD TOOL: Oscilloscope and crystal detector

SPECIFIC TOOL: Loads Bench

5. INSTRUCTIONS :

- Connect equipment as follows:

Crystaldtector

Coupler

RSM 970 MODE SCABINET

50 dB

50 dB

TRIGGER

J 410 MDRPOUTPUT

Oscilloscope

50 TRANSMITTER

CBP REFERENCE SETTING:

- Set with the CBP RSM970S CIRIUS the transmission on full power on 360.- On Scheduling parameters

- I/R map / I/R map (1) / Power map- Number of programmed sectors = 1- Transmission enable = true- Sum attenuation = 0dB- Control attenuation = 0dB

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PULSES CHARACTERISTICS:

P1-P3

Using the CBP RSM970S CIRIUS, select an interrogation mode:Select Scheduling parameters.

Operational patternCheck that the Number of scans for Mode interlacing = 1Check that the Number of azimuthal areas = 1Select Number of period = 1Select Kind = All CallSelect AC interrogations for scan 1:

AC interrogations P1P3M1 (M2, M3A, MC)

Change the interrogation mode and control the spacing between P1 and P3 for each mode

(116) P1P3M1 / Note the result(117) P1P3M2 / Note the result(118) P1P3M3A / Note the result(119) P1P3MC / Note the result

Check the P1 P2 P3 pulse width.

(120) P1 Width / Note the result(121) P3 Width / Note the result(122) P2 Width / Note the result

Check the P1 P2 Spacing

(123) P1 P2 Spacing / Note the result

Repeat the test on channel 2.

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MEASUREMENT PROCEDURE SHEET Nr. 4 S 1/2

1. EQUIPMENT OR MAIN ELEMENT INVOLVED: MODE S TRANSMITTER

2. TESTED FUNCTION: PULSES WIDTH, MODE S

3. PURPOSE: Check the MODE S modes and the width of transmittedpulses.


STANDARD TOOL: Oscilloscope and crystal detector


5. INSTRUCTIONS:


Crystaldtector

Coupler


50 dB

50 dB

TRIGGER

J 410 MDRPOUTPUT

Oscilloscope

50 TRANSMITTER

CBP REFERENCE SETTING:

- Set with the CBP RSM970S CIRIUS the transmission on full power on 360.- On Scheduling parameters

- I/R map / I/R map (1) / Power map- Number of programmed sectors = 1- Transmission enable = true- Sum attenuation = 0dB- Control attenuation = 0dB

Only for the mode S configuration

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P1P3P4SM3A

(124) Check the P1-P3 pulse spacing.(125) Check the P3-P4 pulse spacing.(126) Check the P1 pulse width.(127) Check the P3 pulse width.(128) Check the P4 pulse width.


P1P3P4LM3A

(129) Check the P1-P3 pulse spacing.(130) Check the P3-P4 pulse spacing.

(131) Check the P1 pulse width.(132) Check the P3 pulse width.(133) Check the P4 pulse width.


P1P2P6UF11

(134) Check the P1-P2 pulse spacing.(135) Check the P2-P6 pulse spacing.

(136) Check the P1 pulse width.(137) Check the P2 pulse width.(138) Check the P6 pulse width.

Repeat the same test on channel 2.

Case of P5 on Control

(139) Check the P5 leading edge /P6 synchro phase rev.(140) Check the P5 Width.


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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: TRANSMITTER

2. TESTED FUNCTION: TRANSMITTED SIGNAL POWER

3. PURPOSE: Check nominal power


STANDARD TOOL: OscilloscopePeak Power Meter


5. INSTRUCTIONS:

MEASUREMENT BLOCK DIAGRAM

Connect equipment at RFU relays output as follows:

TRANSMITTER


POWER

SENSOR

PEAKPOWERMETER

50 dBRFU

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IMPORTANT : All these measurements will be done on Loads.

POWER MEASUREMENT

Select channel 1 ON LINE.

Set the transmission full power on 360with the CB P.On Scheduling parameters

I/R map / I/R map (1) / Power mapNumber of programmed sectors = 1Transmission enable = trueSum attenuation = 0dBControl attenuation = 0dB

Select Scheduling parameters.Operational pattern

Check that the Number of scans for Mode interlacing = 1Check that the Number of azimuth areas = 1

Select Number of period = 1Select Kind = All CAllSelect AC interrogation for scan = 1:

AC interrogations = P1P3M3A

5.1 SSR CASE

(141) Check on the SIGMA channel the peak power value.

(142) Check on CONTROL channel the peak power value.

Repeat the test on Channel 2

5.2 MODE S CASE

(143) With the CBP change the parameters.

Select AC interrogations = P1P3P4SM3A. - Full power ISLS

- Read the output power on the peak power meter on .


Select AC interrogations = P1P3P4LM3A- Full power ISLS

Read the output power on the peak power meter on .


Select AC interrogations = P1P2P6UF11- Full power ISLS

Read the output power on the peak power meter on

(146) Read the output power on the peak power meter on for one mode S case.


Only for the mode S configuration

For both configuration

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5.3 POWER ATTENUATION

Set an attenuation of 2 dB on and channelOn Scheduling parameters


Read the output power on the peak power meter on and channels.

Using the same menu

Set an attenuation of 4dB on and channel

Check the effect of the output power on the peak power meter on and channels.





Set an attenuation of 10dB on and channelCheck the effect of the output power on the peak power meter on and channels.



(147) Effect on

(148) Effect on

Repeat the test on Channel 2.


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5.4 SECTORS AND SAFETY CHAIN:

POWER ATTENUATION ON SECTOR BASIS

Using the CBP RSM970S CIRIUS function

Select 2 sectors.

Set an attenuation of 6dB on and channel from 0 to 180 Set a silence mode from 180(149) Check the attenuation on sector basis.


TRANSMISSION OFF

Switch off the transmission via the CBP RSM970S CIRIUS terminal local or RCMS.

CBP RSM970S CIRIUS menu:Key parameters

Transmission enabled= False

(150) Check that transmission is OFF on the peak power meter and RCMS.


SAFETY CHAIN

Switch ON the transmission

Key parametersTransmission enabled= True

Activate the safety chain (switch OFF the antenna rotation)

Check that transmission is OFF on the scope and RCMS.

Deactivate the safety chain (Switch ON the antenna rotation)

(151) Check that transmission return to ON.



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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: TRANSMITTER

2. TESTED FUNCTION: II SLS FUNCTION

3. PURPOSE: Check the correct operation of IISLS


STANDARD TOOL: OscilloscopePeak Power Meter


5. INSTRUCTIONS:


Crystaldtector

Coupler


50 dB

50 dB

TRIGGER

J 410 MDRPOUTPUT

Oscilloscope

50 TRANSMITTER

IMPORTANT : All these measurements will be done on Loads.

Select channel 1 ON LINE.

Set transmission full-power on 360with the CBP.On Scheduling parameters


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IISLS

Select Scheduling parameters.Operational pattern

Check that the Number of scans for Mode interlacing = 1Check that the Number of azimuthal areas = 1Select Number of period = 1Select Kind = All CallSelect AC interrogation for scan 1

AC interrogations P1P3M3A

PROCEDURE

Activate the IISLS mode.

On Scheduling parameters.Select I/R map / I/R map (1) / IISLS map .

Number of programmed sectors = 1IISLS enable = trueControl P1 attenuation = 0 dB

The measurement is performed at the output of the RFU relays.

(152) Read the spacing between pulses P1 and P2 on the oscilloscope.

(153) Measure the width of transmitted pulse P1 at 50 % of the HF amplitude.(154) Measure the width of transmitted pulse P2 at 50 % of the HF amplitude.

Repeat this operation on Channel 2

ATTENUATION IN IISLS MODE

Program an attenuation on the ratio P1/P2 on 3 sectors:

Select I/R map / I/R map (1) / IISLS map.Number of programmed sectors = 3

from 0 to 120 , ratio = 2 dBfrom 120 to 240 , ratio = 4 dBfrom 240 to 360 , ratio = 6 dB

(155) Check with the scope the presence of 3 P1 attenuation.

(156) Check with the scope the presence of 3 sectors.

Repeat this operation on Channel 2

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1. EQUIPMENT OR MAIN ELEMENT INVOLVED: RECEIVER

2. TESTED FUNCTION: RECEIVER SENSITIVITY

3. PURPOSE: Measurement of the receiver minimum signal


STANDARD TOOL: OscilloscopePulse generatorL band RF generator

5. INSTRUCTIONS:

- Connect the equipment as follows:

TRIGGER J410RECEIVER

MDRP

RX

J 302 Log

J 303 Log

J 326 Log

RF GENERATOR

PULSEGENERATOR

Attenuator

OSCILLOSCOPE

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**Warning**SWITCH OFF TRANSMISSION ON BOTH RADAR CHANNELS

ALL THE RF INJECTIONS SHALL BE DONE AT THE TRC CABINET INPUTS

SENSITIVITY:

Select the following settings on the generator:

- 1090 MHz- internal modulation (pulse gen)- pulse width = 460 ns- delay = 30 s- triggered by radar (trigger J410 connect to pulse input of generator)

- Used Power Meter to calibrate the RF generator so as to obtain -20dBm at input- Decrease the RF level.

- Note the RF pulse level at J302 ( on receiver) until pulse is barely visible (TANGENTIAL SENSITIVITY).

- Repeat the test for (J303) and (J 326)

Test:

(157) Sensitivity on Sum.(158) Sensitivity on Control(159) Sensitivity on Delta

TANGENTIAL SENSITIVITY

PULSE

RECEIVER NOISE


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2. TESTED FUNCTION: RECEIVER BANDWIDTH

3. PURPOSE: Measurement of the receiver bandwidth


STANDARD TOOL: OscilloscopePulse generatorL band RF generator

5. INSTRUCTIONS:

- Connect the equipment as follow:

TRIGGER J410

RECEIVERMDRP

RX

J 302 Log

J 303 Log

J 326 Log

RF GENERATOR

PULSEGENERATOR

Attenuator

OSCILLOSCOPE

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**Warning**

SWITCH OFF TRANSMISSION ON BOTH RADAR CHANNELS

BANDWITH:

Select the following settings on the generator:

- 1090 MHz- power = - 80dBm- pulse width = 460 ns- delay = 30 s- triggered by radar (trigger J410 connect to pulse input of generator)

- Connect the RF generator at input cabinet.

- Connect the oscilloscope to J302 (log output of the receiver MDRP).

- Take a reference level on the oscilloscope (RF signal to -80 dBm)

- Increase the RF signal to -77 dBm.

- Scan the RF frequency to find back the reference level

- The frequency span gives the 3 dB bandwidth around 1090 MHz.

- Performed the measurement for:

(160) (J302)(161) (J326)(162) (J303)


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2. TESTED FUNCTION: TEST OF TVBC LAWS EFFICIENCY

3. PURPOSE: Verification of sector-based desensitization laws.


STANDARD TOOL: SMS Site Monitor

5. INSTRUCTIONS:

This test will be performed on the local SMS Site Monitor.

MEASUREMENT BLOCK DIAGRAM

TEST OF DESENSITIZATION LAW EFFICIENCY

Law A

Law B

Effect of desensitization laws

range

Amplitude

IBIS


SMS

SITE MONITOR

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REMARK:

-This test is optional and only available in case of presence of Site monitor type SMS or equivalent.- If the site conditions are not compatible with this test (Range Radar to Site monitor or accessdifficulty), the test can be made in the same conditions as the factory with HF generator.

FOR THE MODIFICATION OF RANGE OF THE SMS SITE MONITOR YOU NEED THEAUTORISATION OF THE LOCAL AUTORITY.

- On CBP RSM970S CIRIUS menu key parameters :

- Change LLT SM1 and LLT SM2 = is not essential in order to have no alarm during the test.

- Using the CBP RSM970S CIRIUS tools select a fixed TVBC law on 360. Typical law = 3

- Scheduling parameters.

- I/R map / I/R map (1) / TVBC map.- TVBC map content.- TVBC law selection in sector (1).

(163) Defined the law number with the CBP RSM970S CIRIUS - ( Typical law 3 for this test )

Using the Site Monitor, select the range at 20NM.Increase the attenuation on the Site Monitor in order to see it disappearing on IBIS display.

(164) Note the last LOG level on IBIS.

Then adjust the Site Monitor range at 40NM

Increase the attenuation on the Site Monitor in order to see it disappearing on IBIS display.(165) Note the last LOG level on IBIS.

(166) Check the difference of attenuation between the 2 ranges of the Site Monitor.


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2. TESTED FUNCTION: TEST OF RSLS FUNCTION

3. PURPOSE: Check the RSLS selection.


5. INSTRUCTIONS:

This test is performed with the Site RSLS adjustment and the operational pattern of interrogation.

This check will be done on one SSR plane with good reception conditions (level > than 80 dBm, range 50 to100NM, 20000 to 30000 feet).

Modified the Scheduling parameters; Operational pattern in order to get a SSR pattern interrogation type All callMode A and Mode C.

Then:On the CBP RSM970S CIRIUS tool

Select LD outputLD output selectionReply reports output = True

On the IBIS, select a plane with the mouse

Select Kinematics page:(167) Note the selected plane range(168) Note the selected plane flight level (Height).

Select Plot characteristics page:(169) Note the selected plane LOG level (Amplitude).(170) Read the number of received replies and note it.

On the CBP RSM970S CIRIUS:Select Reception parameters

RSLS Control

And note the values of the 4 parameters.

(171) DIFF_VALUE(172) DIFF_VALIDATION(173) CONTROL_VALUE(174) CONTROL_VALIDATION

Repeat the measurement on Channel 2

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2. TESTED FUNCTION: INTERNAL PLOT SSR AND MODE S.

3. PURPOSE: Check the internal SSR and Mode S test plots.


5. INSTRUCTIONS:

Used the site parameters

On Channel 1:

5.1 SSR Internal test plot:

Using the CBP RSM970S CIRIUSTTG parameters / SSR TTG generation

Is generated = Always

Check the SSR TTG position and SSR TTG characteristics.Compare the selected parameters and the positioning of the tracks on IBIS.

(175) Mode A,(176) Range

(177) Azimuth(178) Mode C (Altitude)(179) Change some parameters and check the new value on IBIS.

5.2 MODE S Internal test plot:

Using the CBP RSM970S CIRIUSTTG parameters / MS TTG generation

Is generated = Always

Check the MS TTG position and MS TTG characteristics.

Compare the selected parameters and the positioning of the tracks on IBIS.

(180) Mode S Address(181) Range(182) Azimuth(183) Amplitude Value(184) Change some parameters and check the new value on IBIS.


Only for mode S configuration

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2. TESTED FUNCTION: SSR AND MODE S SMS Site Monitor

3. PURPOSE: Check the external SSR and Mode S test plots


5. INSTRUCTIONS:

Used the site parameters

Check that there is no SMS Site Monitor alarm on RCMS or SDPT.

5.1 For SSR

Site Monitor (Channel 1).

Select on the IBIS the Site Monitor channel 1.

(185) Note the mode A(186) Note the mode C(187) Note the Range(188) Note the azimuth.(189) Note the LOG level



(190) Note the mode A(191) Note the mode C(192) Note the Range(193) Note the azimuth.(194) Note the LOG level

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5.2 For Mode S



(195) Note the Mode S address(196) Note the Range(197) Note the Azimuth(198) Note the LOG level



(199) Note the Mode S address(200) Note the Range(201) Note the Azimuth(202) Note the LOG level



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2. TESTED FUNCTION: BDS EXTRACTION

3. PURPOSE: Select two different BDS extraction.


5. INSTRUCTIONS:

The station must be operational with a Mode S pattern (not available on SSR Mode).The BDS extraction is possible only on a transponder with a level greater or equal to 1 (COM >=1).

- On CBP RSM970S CIRIUSLD output / LD output selectionReply reports output = True

- Use the CBP RSM970S CIRIUS tool to select the BDS extraction.Enhanced surveillance

Automatic GICB extractionNumber of BDS = 2

BDS identifier = 10 (Data link capacity)Extraction priority = 14Extraction period = 1Constrained periodicity = FalseAsynchronous update enable = True

BDS identifier = 30 (ACAS)Extraction priority = 14Extraction period = 1Constrained periodicity = FalseAsynchronous update enable = True

- Switch off the transmission- Wait that all tracks disappear- Switch on the transmission

On the IBIS

Use the mouse to select a track (Aircraft)

Select BDS page:(203) (204) Check the BDS 10 extraction at each scan (BDS extracted in the scan)

Select Mode S page:(205) Check the BDS 30 extraction (ACAS information)



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2. TESTED FUNCTION: OFF LINE TEST

3. PURPOSE: Check the result of the off line test.


5. INSTRUCTIONS:

- Set the channel 1 stand-by (to load).

- For this test the DPC-PC must be without alarm.

- Using the RCMS CONFIGURATION page: select Maintenance mode, and click on send button.

- Using the RCMS SPECIAL CONTROL page: click on send at the front of OFF LINE TEST.

(206) Wait about 5 minutes (DPC-PC reboot) and check there is no alarm.


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2. TESTED FUNCTION: AUTOMATIC OR MANUAL SWITCHING

3. PURPOSE: Check the switching to standby unit in case of operational unitrequest or failure.


5. INSTRUCTIONS:

MANUAL SWITCHING

- Set the Channel 1 On-Line (to antenna)

- Request a switching via CBP RSM970S CIRIUS terminal or LTM and check that channel 2 is On-Line. The switchingis possible only from the channel TO LOAD.

Procedure:

From the CBP:- Select Command- Select Commands to radar- I/R Channel switchover- Send

From the LTM:- ON THE CHANNEL TO LOAD.- Open CONFIGURATION page- Modify CONFIGURATION STATE from TO LOAD to ANTENNA

(207) Check the result on LTM and CBP and switch back to channel 1.

AUTOMATIC SWITCHING

- Set both channels in operational.- Set Channel 1 on-line (to antenna).- On the channel on-line disconnect J8 on the driver (local oscillator)

(208) Check there is an alarm on Channel 1.- Channel 1 AVAILABLE = NO- Channel 2 CONFIGURATION STATE: TO LOAD- Channel 1 CONFIGURATION STATE: TO ANTENNA

- Reconnect plug J8, make a reset failure and check that channel 2 stay On line.


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2. TESTED FUNCTION: ENCODER FAILURE

3. PURPOSE: Check the detection of failure and switching when encoder 1or 2 is missing on one channel.


5. INSTRUCTIONS:

- Set both Channels to operational mode- Select Channel 1 TO ANTENNA

- In the TOM cabinet ,disconnect the cable W116 from the multi-socket MA N1-

(209)Check that

- An alarm raise on Channel 1- A switchover occur, the Channel 2 is now TO ANTENNA.

-Reconnect the cable W116 on the multi-socket MA N1 and wait until that all failures disappeared.

Operated in the same way for switching from channel 2 to channel 1(In the TOM cabinet, disconnect the cable W117 from the multi-socket MA N2)

-Reconnect the cable W117 on the multi-socket MA N2 and wait until that all failures disappeared.

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2. TESTED FUNCTION: TIME STAMPING (OPTION)

3. PURPOSE: Check the time stamping function

4. RECOMMENDED TEST TOOLS: IBIS

5. INSTRUCTIONS:

The time stamping function is optional

(210) / On the NTP screen, check the presence of the following information:

- GPS : NORMAL OPERATION- DATE : DATE OF THE DAY- TIME : CORRECT TIME INFORMATION- Check that Ref. Time, Time Service and Network led are green.

(211) / Then press and select Reference Time (valid with OK)

Select Info GPS(OK) and GPS position(OK) and note the following information:

- Latitude- Longitude

- Altitude (use or to change the unit)

(212) / Then press esc and select GPS satellites and note the following information:

- Number of satellite IN VIEW- Number of Satellite GOOD

(213) / Test on IBIS

Then check on IBIS the presence of time stamping on tracks for channel 1


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