宇宙科学研究所報告
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- ひろき しげい
- 7 years ago
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1 MV CNE MV ING : Inertial Navigation Guidance MSII FRIG : Floated Rate Integration GyroSFAP MV FOG : Fiber Optic Gyro CPU IMU : Inertial Measurement Unit ING MV FOG MV FOG IMU CPU I/O 1.2. MV ING IMU
2 IMU ING IMU IMU RG ING ING MNTVC SMRC ON/OFF LITVC SMRC ON/OFF SMSJ ON/OFF MNTVC SJ ON/OFF ING NAV START
3 BCONT START BCONT START BCONT START RG PPPact YYYact RS CMD A CMD A BMNTVC ON/OFF I/O PKG ON/OFF 1.3. ING degσ degσ degσ degσ degσ ms m/sσ ms mσ mσ mσ ms
4 B deg/s ms BP,Y G ms BIMU P,Y BIMU R deg/s deg/s ms ms BIMU G ms 1.4. ING ING IMU PKG CPU PKG BI/O PKG BI/O PKG BI/O PKG BR/G PKG BACC PKG ING
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7 IMU PKG IMU PKG FOG CPU PKG ING P,Y R deg deg deg/s deg/s arcsec/pulse ms Hz G m/s/pulse ms Hz ING V W A WDH mm kg
8 IMU PKG CPU PKG ING ING ai/o PKG bcpu PKG IMU IMU RS RG MC ROM RAM CPU-IMU, I/O PKG ING V WDH MFLOPSMHz MIPSMHz KByte MByte port KByte/s/port bit/port bit/port bit/port port Kbit/s port Byte/ms ch ch W A mm kg
9 / I/O PKG I/O PKG I/O PKG I/O PKG CPU PKG CPU PKG I/O PKG I/O PKGCPU PKG ING V V WDH port KByte/s/port bit/port bit/port bit/port ch ch ch ch W A A mm kg
10 / BR/G PKG BR/G PKG I/O PKG
11 deg deg/s V deg/s deg/s/v /FS Hz V W A WDH mm kg BACC PKG BACC PKG I/O PKG
12 deg G V mg G/V /FS Hz V W A WDH mm kg 1.6. I/O PKG V ING BATV / I/O PKG VV
13 V V V IMU PKG BV CPU PKG BV BI/O PKG BV BV BV BI/O PKG BV BV BACC PKG BV BI/O PKG BV BV BR/G PKG BV IMU PKG CPU PKG I/O PKG V CPU PKG B ACC PKG B R/G PKG I/O PKG B V B S/A / RAM
14 ING RG RS 1.8. ING N X Y Z G X MV Y X
15 Z K X Y Z B X Y Z X Y 1.9. ING ING
16
17
18
19 ING
20 RG XsXs deg/pulse XsXs deg/pulse XsXs deg/pulse ING DD msms
21 IMU ANCActive Nutation Control SMSJ SJ BBQ MTVC MMNTVC MMNTVC BI/F PWR DC/DC CPU MHz MHz BCONT RG [deg/pulse] SJ MV
22 2. ING : Inertial Navigation Guidance ANCActive Nutation Control 2.1. X Y ING JOBCPU PKG PWR ON Xhrmin JOBIMU PKG PWR ON IMU Xhrmin JOBM/T DATA SET Xhrmin JOBGYRO BIAS Xmin JOBGYRO BIAS SET JOBGYRO BIAS DC Xmin NAV START Xsec Xsec ST/CTRKT Xsec AZMdegELVdeg ING IMUInertial Measurement Unit
23 IMU ING φdeg IMU Y Ydeg IMU Pitch/Yaw AZM/ELV AZM AZMdeg No. deg ING deg ING deg // // φ
24 ING X Pdeg Ydeg Rdeg No. XTimesec Pitchdeg Yawdeg Rolldeg
25 No EPT sec sec NAV START X BCONT START X BCONT START X BCONT START X PITCH YAW sec pulse pulse sec RC XX XX RC XX X RC XX MTVC MTVC / X X Xdegdeg Xdegdeg BSMRC BSMRC X X XdegX deg MTVC MTVC / X X / Xdeg BSMRC
26 BSMRC X X XdegX deg SMSJ SMSJ X XX MTVC MTVC / X X M degdegxdeg degdeg X XHzdegp p SJ am SJ M X X degxdegx degx bm SJ M XXHi Thruster Mode X XLow Thruster Mode deghi Xdeg cm SJ M X X degxdegx degx/ Xdeg deg X XRG MTVC ANC MVANCActive Nutation Control
27 XX
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30
31 2.4. ING NK degdegm ING KK ING msecmsecxtimesecing sec NKMV/MUSESB a akk degbk Z ING b N ING a XX X bx m/sm/s ING deg X Verr sin m/sec XTIMEsec Vxm/sec Vym/sec Vzm/sec
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33
34 ING : Inertial Navigation Guidance SJ ANCActive Nutation Control 3.1. X Y ING JOBCPU PKG PWR ON Xhrmin JOBIMU PKG PWR ON IMU Xhrmin JOBM/T DATA SET Xhrmin JOBGYRO BIAS Xmin JOBGYRO BIAS SET JOBGYRO BIAS DC Xmin NAV START Xsec ST/CTRKT Xsec Xsec AZMdegELVdeg ING
35 IMUInertial Measurement Unit IMU ING φdeg IMU Y Ydeg IMU Pitch/Yaw Pitch degazm/elv AZM deg AZM No. deg ING deg ING deg CN // // //
36 φ ING X Pdeg Ydeg Rdeg
37 No XTIMEsec Pitchdeg Yawdeg Rolldeg
38 No EPT sec sec NAV START X BCONT START X BCONT START X BCONT START X **** EPT T sec PITCH YAW pulse pulse sec RC XX XX RC XX X RC XX X MTVC MTVC / X X Xdegdeg BSMRC BSMRC X X XdegX deg
39 MTVC MTVC / X X / Xdeg BSMRC BSMRC X X XdegX deg SMSJ SMSJ X XX MTVC MTVC / X X M degdegxdeg deg SJ am SJ M X X degdeg deg bm SJ M XX XX cm SJ MX XX XX XX ANC
40 MVANCActive Nutation Control XANC
41
42 3.4. ING NK degdegm ING K msecing msec NKMV/PlanetB aing KX MV degb X
43
44 4. ING : Inertial Navigation Guidance 4.1. X ING JOBCPU PKG PWR ON Xhrmin JOBIMU PKG PWR ON IMU Xhrmin Xhrmin JOBM/T DATA SET Xhrmin JOBGYRO BIAS X minx JOBGYRO BIAS SET minxmin JOBGYRO BIAS DC Xmin NAV START Xsec ST/CTRKT Xsec Xsec AZMdeg ELVdeg ING IMUInertial Measurement Unit
45 IMU ING AZM AZMdeg No. deg ING deg ING deg ING X Pdeg Y deg Rdeg No EPT sec sec NAV START X X BCONT START X X BCONT START X X
46 No XTIMEsec Pitchdeg Yawdeg Rolldeg
47 sec pulse sec XX P XX RC XX Y XX XX P X RC XX P X XX Y X RC X Y X RCdeg/pulseRCdeg /pulse MTVC TVC MTVC / X XX ING X BSMRC / SMRC /BSMRC X XX ING X CW SMRC MTVC MTVC /X X degdeg X deg RG
48 BSMRC BSMRC X X deg X deg SMSJ SMSJ X XX MTVC MTVC / X X M degdegxdeg deg degdeg SJ am SJ M X X degdeg deg bm SJ M XX XX Xdeg SJ cm SJ MX XX XX XX XX SJ XX XX XX SJ X XX XX
49 XX XX XX
50
51 4.3.4.
52
53
54 4.4. ING NK degdegm ING K msecing msec NKMV/PlanetB ING KY MV deg RG
55 ING B RG BRG deg deging RG ING timesec Pitchdeg Yawdeg ING RG ING B RG ING ING deg
56 ING timesec Pitchdeg Yawdeg ING RG
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慣性運動計測機器 クロ ス ボ ー株 式 会 社 Crossbow Japan Ltd. MEMS 3 1 X Y Z 3 RS-232 Windows Gyro-View Nav-View GPS NAV420 3 AHRS400 VG400 6 IMU400 (AHRS) TEL: 06-6489-5922 FAX: 06-6489-5910 E-MAIL: sales@xbow.jp WEB:
3 m/sec 8.35 39.06 3.22 2.15 13.72 52.78 15.00 2.12 2.69 12.62 27.62 3 m/ 772 79 68 263 410 1,182 3 m/sec 3.87 0.63 8.00 3.12 1.38 12.50 12.50 2.00 2.50 1.00 5.50 5.50 m/ 105 122 20 247 247 3 m/sec 0.23
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1 211022 2 11150 211022384 3 1000 23% 77% 10% 10% 5% 20% 15% 40% 5% 3% 8% 16% 15% 42% 5% 6% 4 =1000 = 66 5 =1000 = 59 6 52%(42% 1000 7 56% 41% 40% 97% 3% 11%, 2% 3%, 41 7% 49% 30%, 18%, 40%, 83% =1000
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