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FLIGHT INSPECTION CENTER Japan Civil Aviation Bureau

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Page 1: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

FLIGHTINSPECTIONCENTER

Japan Civil Aviation Bureau

Page 2: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

The summary of

The Flight InspectionData Management system

Page 3: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

1. Introduction2. Structure3. Functions4. Conclusion

Agenda

Page 4: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

1. Introduction

Page 5: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

1. Introduction

Page 6: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

1. IntroductionFIDM has following main functions to operate flight inspection efficiently.

FIDMsystem

Main functions - Coverage simulation- RNAV analysis- Visualization of relationship

between terrain and radio waveand more.

Some of these are explained in latter slides.

Page 7: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

2. Structure

Page 8: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

2. Structure

FIDM structure

OPERATION PROCESSING UNIT

DATABASEMANAGEMENT UNIT

LAPTOP TYPEINFORMATION DISP

LAPTOP TYPEINFORMATION DISP

….and more

InternetLAPTOP TYPEINFORMATION DISP

Flight procedure designers

Research institutes

External users

FI-dataObstacle data

AIP dataTerrain data

VPN

web

web WEB SEVER

Page 9: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

2. Structure

The data used for display

Obstacle data

Terrain data

FI-data

AIP data or Procedure design data

AIP data

FIX

FIX

- FI data- AIP data- Terrain data- Obstacle data- Procedure

design data

are utilized for display

Page 10: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

2. Structure

FI-data outline

eqmAHRS:: eqmAHRS:: eqmAHRS:: eqmALT1:: eqmALT1:: eqmDME1:: eqmDME1:: eqmDME1:: eqmDME1::sigAHRSMasigAHRSPitsigAHRSRosigALTBarosigALTPressigDMEAGCsigDMECh1sigDMECh1sigDMECh1

TIMESLOT (Double) (Double) (Double) (Integer) (Integer) (Double) (Double) (Double) (Text)77616 245.2972 0.726506 3.243706 2980 3316 149.1965 14.7277 116.6577617 245.3192 0.826489 3.109005 2980 3316 149.1265 14.71988 116.65 HCE77618 245.3577 0.89741 3.056694 2980 3316 149.3227 14.71875 116.6577619 245.4071 0.911819 2.956152 2980 3316 149.9429 14.71875 116.65 HCE77620 245.4401 0.900341 2.890125 2980 3316 150.2005 14.71875 116.6577621 245.4401 0.881117 2.918935 2980 3316 149.5453 14.71207 116.65 HCE77622 245.4565 0.848522 2.932446 2980 3316 149.0542 14.70425 116.6577623 245.4675 0.824864 2.922853 2980 3316 148.0579 14.70313 116.65 HCE77624 245.4785 0.812932 2.922386 2980 3316 146.3769 14.69645 116.6577625 245.4785 0.802292 2.94391 2980 3317 143.6359 14.69531 116.65 HCE77626 245.473 0.811946 2.924533 2980 3318 141.5447 14.68863 116.6577627 245.4565 0.833447 2.851078 2980 3318 141.2072 14.68081 116.65 HCE77628 245.4291 0.877716 2.739029 2980 3318 140.3505 14.67969 116.6577629 245.3467 0.923082 2.581313 2980 3318 137.9697 14.67301 116.65 HCE77630 245.3467 0.961462 2.344904 2980 3318 135.3144 14.67188 116.6577631 245.3082 0.966797 2.132141 2980 3318 134.3709 14.66519 116.65 HCE77632 245.2643 0.946175 1.791243 2980 3318 133.3917 14.66406 116.6577633 245.2533 0.891036 1.489998 2980 3318 130.2294 14.65738 116.65 HCE77634 245.3192 0.81146 1.339683 2980 3318 127.7882 14.64956 116.6577635 245.3192 0.735033 1.301503 2980 3318 126.9489 14.64844 116.65 HCE77636 245.3796 0.725098 1.296387 2980 3318 127.2892 14.64175 116.6577637 245.4456 0.725098 1.296387 2980 3318 128.4282 14.64063 116.65 HCE77638 245.5005 0.6708 1.253133 2980 3318 130.0326 14.63394 116.6577639 245.6488 0.5696 1.321295 2980 3318 134.1957 14.63281 116.65 HCE77640 245.6488 0.49284 1.484411 2982 3318 138.9965 14.63281 116.6577641 245.7202 0.463346 1.704941 2982 3318 143.1768 14.62613 116.65 HCE77642 245.7697 0.513568 1.942009 2982 3318 145.6662 14.625 116.6577643 245.8136 0.636199 2.053303 2982 3318 148.0427 14.61832 116.65 HCE77644 245.8466 0.78434 2.031807 2982 3318 149.0663 14.6105 116.6577645 245.8466 0.928014 2.002972 2982 3318 148.1038 14.60938 116.65 HCE77646 245.863 1.025834 2.029756 2982 3318 147.0699 14.60269 116.6577647 245.885 1.085534 2.084681 2982 3318 144.8258 14.60156 116.65 HCE77648 245.885 1.109687 2.098377 2982 3318 144.8948 14.59488 116.6577649 245.885 1.131899 2.043226 2982 3318 145.3573 14.59375 116.65 HCE77650 245.885 1.141503 2.03358 2982 3318 146.6031 14.59375 116.65

Flight Inspection data

FI-data contains exceeding 100 signals

- GPS information- Aircraft information- Signals from ground

navigation facilities

These are outputted on 10Hz

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others data outline

2. StructureObstacle tyLatitude Longitude Height ElevationTOWER 434625.6 1422623 126 261TOWER 425509 1431331 83 119TOWER 440008.7 1441427 83 268TOWER 434905.7 1435213 83 213TOWER 442040.3 1422833 83 199TOWER 430340.7 1412122 146 162.5TOWER 434618.6 1422631 126 238TOWER 425527 1431156 71.5 110.5TOWER 432006.1 1453544 67 115STACK 425517 1430442 70 139.45MONUMEN 430325.8 1412948 100 155STACK 423809 1413947 77.4 85.4TOWER 425900.1 1442228 77.2 79.4

mid codeIdgeoLat geoLong txtNameDMEM00000001 KNE 342548.31N 1351506.42E CIVIL AVIATION BUREAU, MLITDMEM00000005 IKD 342505.55N 1351358.31E CIVIL AVIATION BUREAU, MLITDMEM00000006 IKN 342603.33N 1351524.41E CIVIL AVIATION BUREAU, MLITDMEM00000007 IKJ 342551.96N 1351228.41E CIVIL AVIATION BUREAU, MLITDMEM00000008 IKW 342701.15N 1351411.05E CIVIL AVIATION BUREAU, MLITDMEM00000009 IKX 262225.79N 1264308.03E CIVIL AVIATION BUREAU, MLITDMEM00000010 IMY 244712.74N 1251801.01E CIVIL AVIATION BUREAU, MLITDMEM00000012 HKE 354851.00N 1402217.81E CIVIL AVIATION BUREAU, MLITDMEM00000013 NRE 354656.44N 1402145.13E CIVIL AVIATION BUREAU, MLITDMEM00000014 SND 355605.37N 1395853.23E CIVIL AVIATION BUREAU, MLITDMEM00000016 YNE 242753.72N 1225951.86E CIVIL AVIATION BUREAU, MLITDMEM00000017 IYN 242750.22N 1225805.42E CIVIL AVIATION BUREAU, MLITDMEM00000018 IOK 261107.00N 1273841.98E CIVIL AVIATION BUREAU, MLITDMEM00000019 HWE 414626.51N 1404955.98E CIVIL AVIATION BUREAU, MLITDMEM00000020 IKF 354615.89N 1402207.71E CIVIL AVIATION BUREAU, MLITDMEM00000021 IYQ 354443.18N 1402315.19E CIVIL AVIATION BUREAU, MLITDMEM00000022 ITM 354810.82N 1402253.68E CIVIL AVIATION BUREAU, MLIT

Obstacle data

Terrain data

AIP data(AIXM4.5)

Page 12: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

Airspace box

2. StructureLongitude direction width:

30seconds

Latitude direction width: 30seconds

*

*Height: 100ft step below ALT 5000ft1000ft step at or above ALT 5000ft

- SLOT

12m

Page 13: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

Airspace box

2. Structure

25NM orbit for coverage check

Air spacebox

A = 25NM*2*pi*1/360 =0.44NM ≒ 30 seconds

AA

Page 14: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

3. Functions

Page 15: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

3. Functions

Coverage simulation

‒ Improving clarification and precision of simulated coverage.

‒ Theoretical coverage is corrected by latest FI data.

Page 16: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

FL 450

Line of minimum signal strength

Coverage simulation

3. FunctionsTheoretical Coverage Condition

Page 17: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

Coverage simulation

3. Functions

15NM ORBIT

In case of SS of 15NM orbit data less than expected SS.Coverage is reduced by this proportion.

Coverage simulation

Corrected Coverage Condition

Page 18: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

Coverage simulation

Predicted blind area

3. Functions

Page 19: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

Coverage simulation

3. Functions

Not receivedReceived

Predicted blind area

Page 20: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

Coverage simulation

Not receivedReceived

3. Functions

Corrected blind area

Page 21: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

3. Functions

RNAV analysis

‒ The function applying the multiple coverage simulations.

‒ Critical DME, DME GAP and DMEs LIST constituting RNAV are analyzed.

RNAV5 route in JAPAN

Page 22: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

RNAV analysis

3. Functions

RNAV route by AIXM4.5 orProcedure design data

Coverage simulations

Result Not Critical & DME GAP CriticalDME GAP

And composition DME LIST is displayed

Page 23: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

3. Functions

Visualization of relationshipbetween terrain and radio wave

‒ To grasp the relationship between terrain and radio wave conditions easily.

‒ With this function, it will be possible to prevent from setting a new flight procedure in poor radio wave conditions area.

Page 24: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

3. Functions

Visualization image between terrain and radio wave

Visualization of relationship

Page 25: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

4. Conclusion

Page 26: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

4. Conclusion

FIDM effects

‒ Re-inspection due to the poor signal condition will be reduced by the result of coverage simulation.

‒ Partial of RNAV flight inspection will be omitted by the result of RNAV analysis.

Page 27: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

4. Conclusion

Works to realize these effects

‒ To secure enough flight inspection data amount.

‒ To determine an appropriate modeling formula for coverage simulation.

‒ To Validate for the coverage simulation result.

Page 28: FLIGHT INSPECTION CENTER · Visualization image between terrain and radio wave. Visualization of relationship. 4. Conclusion. 4. Conclusion FIDM effects ‒ Re-inspection due to the

Q&A

Any questions?

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END

Thank you for your attention