JERG-2-500 制御系設計標準 - 安全・信頼性推進部
Contents
1. FDIR Fault Detection Tsolation and Recovery2. 4 C D
3. 4 FDIR
4. 3 6 3 A B C 3 6 3 1
5. TT amp C SE E F 20 JERG 2 500A 2 5
6. c 1 2
7. 1 2 a b
8. FDIR JERG 2 007 3 3 4 3 3 4 1
9. a b c 3 4 5
10. 10 JERG 2 500A
11. 1 2 SEMP 3 3 1 3 1
12. 21 JERG 2 500A 3 2 3 1
13. Ni
14. 3 3 2 10 JERG 2 007 3 3 3 3 3 3 1 2 1
15. H EN Ee TT Spacecraft On orbit Operations Handbook SOCP SOP 1 5 Spacecraft On orbit Checkout Procedure JERG 2 500A Spacecraft Operations Procedure SI SI fF JERG 2 500A 2
16. 2 1 2
17. JERG 2 310 ul mm a r JERG 2 500A BZ TEMAFE OWERK ECSS E 60A Control engineering 14September2004
18. SEMP 18 B JERG 2 500A gt 0 A
19. 3 1 32 JERG 2 500A 3 1
20. Rs
21. AAA
22. FDIR SEMP
23. i y 20 Estimated State 21 Estimator 3 22 Guidance TT
24. 11 Control Performance 1 2 12 Contro1 System 13 Controllability 14 Contro1led Plant
25. 3 6 4 3 6 4 1 1 2 3 3 6 4 2 3 4 1 FDIR 2
26. 2 1 II IV 3 JAXA NASA 1
27. B 28 3 3 2 3 3 3 3 2 4
28. AT x 2 2
29. 1 EE TW ul pa ul 15 JERG 2 500A 1
30. i f A 2 3 2 1 BS JERG 2 500A E
31. T2000 ED let 32 i H 3 4 2 3
32. 3 1 1 JERG 2 310
33. H 4 gt JAXA E JERG 2 500A
34. 2 H W S W H W S W
35. PPP Phased Project Planning PPP AS 1 o B C EM STM
36. 1 2 3 JMR 001B 4 5 6 7 8 9 JMR 005A JERG 2 610 JERG 2 700 10 JERG 2 007 1 3 3 1 JMR 011 JMR 004C HH 1 BDB 06007B 19 1 JMR 006 BDD 06005 JAXA TRD 2 ECSS E 60A Control engineering 14September2004 3
37. 2 ee
38. Pe 1 2 3 5 4 4 29 E E JERG 2 500A 6
39. A B FDIR FDIR A B FDIR a b 26 c 3 2 3 H
40. 3 6 JMR 004 JERG 2 610 oo E E JMR 005 CE BDB 06007 322
41. 3 1 22 Px cc SE 2 JMR 001A JMR 004A JMR 005 JMR 006 JERG 2 610 JMR 011 27AO 7
42. 1 PR F 1 3 1 3 1 2 1 3 2 JAXA JERG 2 500A 1
43. 1 41 1 1 JERG 2 500A
44. CAE ECSS E 60A Control engineering 14September2004 3 4 2 2 2 1 1
45. E ICD JERG 2 500A 3 3 3 3 1 1 2 C B ul
46. 35 H C D i A FDIR 1 1 2 3 5 1H 3 6 3 6 1
47. 1 2 a C A 3 3 2 5 3 3 2 6 3 3 2 7 b
48. HH 3 5 f 6 J 27 E CD
49. I 3 2 2 2 5 1 1 3 3
50. E 0 A B C BBM EM 2 E C D PFM E RE lt 7
51. 17 Desired State 1 2 2 1 E JERG 2 500A 18 Disturbance 1 19 Environment
52. 16 JERG 2 500A 2 3 2 2 2 5 ECSS E 60A Contro engineering 14September2004 17 2 2 0 A JERG 2 500A po EC PF
53. 1 2 3 2 3 3 3 4 2 3 4 2 1 3 3 3 4 2 3 4 2 1
54. 3 Contro1 f 4 Control Command 5 Contro1 Component 6 Control Feedback Control Function 7 8
55. 1 One Fail Operational Two Fail Safe 2 NE JERG 2 500A a et b 2 FDIR F 3 4 E DIR
56. 2 a b GC a 3 I yr kad
57. 7 BOL EOL 3 3 2 8 GPS Global Positioning System GPS GPS GPS 3 3 2 9
58. ICD 9 JERG 2 500A JERG 2 610 3 3 5 2 ICD 3 1 2
59. 32 Simulation 33 Stabi ity Ct Asymptotically stable Asymptotically Stable in the Large NR 34 State 1 2 2 1
60. GNC 2 2 Es 3 lt gt gt lt gt 2 2 DD DD DD 11 JERG 2 500A FDIR 2 1 2 3
61. NT Mons 5 2 3
62. 2 3 3 1 4 1 TT amp C 2
63. JERG 2 700 2 2 r 7 MEOWERKN ECSS E 60A Control engineering 14September2004
64. JERG 2 500A K E 5 FDIR 6 3 6 5 A ED NN NR SOOH SOCP ee SOOH S0CP
65. CR 88912 3 1 JAXA 23 JERG 2 500A 3 1 1 BDB 06007 SEMP 3 1 2
66. LSB 29 Reference State E JERG 2 500A 30 Robustness 1 31 Sensor
67. 1 CRE DD ES a 2 15 Controlled System 16 Controller
68. 3 a b c 3 f g h i 5 4 JERG 2 510A JERG 2 151 JERG 2 153 JERG 2 152 JERG 2 151 HB001 JERG 2 152 HB101 JERG 2 100 HB101 JERG 2 510 HB102 JERG 2 510 HB001 JERG 2 510 HB002 JERG 2 500A k JERG 2 510 HB003 1 4 1 4 1 ECSS E 60A 1 Actuator ul 2 Autonomy
69. 19 2 4 C D JERG 2 500A 2 B B B B B B B
70. 0 A B 8 33 JERG 2 500A 2 E 3
71. 2 3 13 JERG 2 500A 3 3 3 2 2 3 2 1 14 JERG 2 500A TT 2 1
72. 3 3 6 4 3 End to End 1 2 37 3 EGSE 4
73. 23 Implementation 24 Mathematical Model 25 Measured State 26 Navigation 3 27 0bservablity 28 Quantization
74. b 1 0 A B E LA E f 2 C D b 3 4 4 2 3
75. AB 1 2 FDIR 3 4 5 IV CE 42
76. A RR 1 2 1 JAXA TRL 1 2 3 4 5 I JAXA TRL 6 7 JAXA TRL 8 9 40 JERG 2 500A Actual model flight proven through successful mission operations SDacc Actual model flight qualified through test and demonstration ground or SDace 1 Fight Model
77. D B F 1 12 JERG 2 500A 2
78. 38 SOOH SOP i TCD E E qd 1 JERG 2 100 F JERG 2 151 JERG 2 151 HB001 l JERG 2 100 HB101 JERG 2 152 JERG 2 153 JERG 2 152 HB101 JERG 2 500 JERG 2 510 JERG 2 510 HB102
79. 2 3 1 0 FDIR 2 3 3 2 2 1 0 A 1 3 3 2 b JERG 2 151
80. BE JERG 2 500A 1 H ee oe
81. E F 6
82. gt eS FMEA 17 WBS 7 Eb 2 7 2 JERG 2 500A 7 7 2
83. Wl 006 25 JERG 2 500A 19 1 1 11 0 A 1 19 1 2 3 1 12 1 3
84. 3 1 5 1 2 3 1 3 1 6 24 3 3 3 1 7 H 1 Ni
85. EA JR 1 3 2 3 3 2 3 3 2 1 0 A B 1 2 3 4 5 6 7 3 3 2 2 0 A
86. E a aa aa 7 1 3 6 2 3 6 2 1 E gt gt 1 JERG 2 500A BDB 06007 NM NM 7ex
87. 3D Three Dimensiona1 3 A D AOCS A amp D BOL CAD CAE CAS CE D A EGSE EOL FDIR EM FOV GNC GPS H W 1 F ICD LOS MGSE MMI PA PDR PPP PSD RMS SE SEMP STM S W TBD TT amp C SOOH Analogue Digital Conversion Attitude and Orbit Control System Automation and Robotics Beginning of Life Computer Aided Design Computer Aided Engineering Control Algorithm Specification Control Engineering Digital AnalogueConversion Electrical Ground Support Equipment End of Life Failure Detection lsolation and Recovery Engineering Mode Field of View Guidance Navigation and Control Global Positioning System Hardware Interface Interface Control Document Line of Sight Mechanical Ground Support Equipment Man Machine Interface Product Assurance Preliminary Design Review Phased Project Planning Power Spectral Density Root Mean Square Systems Engineer1ing Systems Engineering Management Plan Structural and Thermal Model Software To Be Defined Telemetry Tracking and Command JERG 2 500A
88. CAE 3D CAD CAE H W S W
89. 1 I II I 1 1 0 CE CE AB 2 7 0 2 3 0 3 4 0 4 5 5
90. 2 JERG 2 510 JERG 2 510 HBO03 3 7 3 7 1 3 7 2 1 2 0 a 3 7 3
91. 1 2 3 3 3 4 2 1 2 30 3 3 3 4 3 3 3 5 3 3 5 1 3 2
92. iv 1 1 1 CE Control Engineering FEE 1 3 1 Es 1 O
93. B EMF MM FDIR
94. 1 3 3 2 3 4 3 3 2 1 3 4 4 3 4 4 1 a
95. 3 4 3 3 4 3 1 3 2 1 2 3 2 1 4 5 ul 3 4 3 2 2 2
96. 35 True State 1 2 36 De orbit IM mT MD 1 4 2
97. JERG 2 510 HB002 JERG 2 510 HB003 JERG 2 510 TMO001 JERG 2 500A 4 1 2 3 1 2 0 1 2 bb
98. 3 JERG 2 500A 3 4 3 4 1 2 1 1
99. Contro1l Mode 1 9 Transition of Contro Mode 10 Control Objective r JERG 2 500A
100. 0 IL I 1 CE AB 1 2 2 FDIR 3 3 4 4 5 5 I CE
101. 0 A 0 A 0 A 0 4 0 A H W S W C D
102. 2 1 2 1 1 2 1
103. 36 lt 3 ee JERG 2 500A
104. 2 a 3 1 8 JMR 011 1 9 3 1 10 3 2 1 3 2 7x JMR 0 A
105. 2 3 JMR 001 1 13 1 3 2 4 JMR 004 1 14 1 1 3 2 5 JMR 005 JERG 2 610 JERG 2 500A 3 2 3 2 1 3 1 2
106. 4 2 2 JERG 2 151 3 4 4 3 FDIR 1 3 3 JERG 2 153 1 3 3 2 JERG 2 151 HB001 3 4 2 2 3 4 5
107. demomnstration SDacc 2 Prototype Model demomstration ground or space Enginecrimg Model validation in relevant environmemt Breadhoard Model validation in laboratory environment Analytical and experimental critical function and or characteristic proof of concept Technologw concept and or application formulated Basic principles observed and reported 1 2 4 1 JAXA TRL
108. 2 5 34 1 3 3 2 JERG 2 500A JERG 2 151 JERG 2 151 HB001 JERG 2 153
109. 7 lt A 24 2 i 24 3 24 4 24 5 OD LTODTyY 3 YATyY 24 24 7 8 9 25 10 25 11 25 2 te ea ee nd ec dd sen ol ei et 25 0 EMR 25 25 11 2 OO NEC Po CO OSI CO OI JO27 ROD COA TO CD NRSS 8 wR NO PS NO PS oO PS No PS D
110. JERG 2 500A 25 3 29 A 22 3 2 JAXA JAXA Disclaimer The information contained herein is for general informational purposes only JAXA makes no warranty express or implied including as to the accuracy usefulness or timeliness of any information herein JAXA will not be liable for any losses relating to the use of the information 305 8505 2 1 1 JAXA Japan Aerospace Exploration Agency nw So CO DD JERG 2 500A IE 9 2 12 2 6 12 1
111. o RM PS Do PS Oo Rs Oi OO NO OO PR WO DD 3 ee 2 SS TEE LE RY CPP 53 SS UNP4 BE BD a a DD i DN 2 YR EE 3 1 2 3 1 2 24NRYE NT A pi NN Na DO i JERG 2 500A 34 4 111 FD PR 6 CC 6 6 6 6 6 RR 6 h h lt h h h h lt h D Pp y DD DD DD DMD rr Do JERG 2 500A 38 DWH 38 39
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