JPS6147760B2 - - Google Patents
Info
- Publication number
- JPS6147760B2 JPS6147760B2 JP55131238A JP13123880A JPS6147760B2 JP S6147760 B2 JPS6147760 B2 JP S6147760B2 JP 55131238 A JP55131238 A JP 55131238A JP 13123880 A JP13123880 A JP 13123880A JP S6147760 B2 JPS6147760 B2 JP S6147760B2
- Authority
- JP
- Japan
- Prior art keywords
- axis
- satellite
- angular velocity
- yaw
- roll angle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 238000010586 diagram Methods 0.000 description 6
- 230000004044 response Effects 0.000 description 4
- 230000003321 amplification Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 238000013016 damping Methods 0.000 description 3
- 238000003199 nucleic acid amplification method Methods 0.000 description 3
- 239000002131 composite material Substances 0.000 description 2
- 230000035764 nutrition Effects 0.000 description 2
- 235000016709 nutrition Nutrition 0.000 description 2
- 230000001052 transient effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000013598 vector Substances 0.000 description 1
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP55131238A JPS5755300A (en) | 1980-09-20 | 1980-09-20 | Triaxial satellite attitude controller |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP55131238A JPS5755300A (en) | 1980-09-20 | 1980-09-20 | Triaxial satellite attitude controller |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5755300A JPS5755300A (en) | 1982-04-02 |
JPS6147760B2 true JPS6147760B2 (en]) | 1986-10-21 |
Family
ID=15053229
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP55131238A Granted JPS5755300A (en) | 1980-09-20 | 1980-09-20 | Triaxial satellite attitude controller |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5755300A (en]) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3017820U (ja) * | 1994-12-08 | 1995-11-07 | 株式会社大紅 | 車輪に付着した泥土の除去装置 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4521855A (en) * | 1981-07-27 | 1985-06-04 | Ford Aerospace & Communications Corporation | Electronic on-orbit roll/yaw satellite control |
-
1980
- 1980-09-20 JP JP55131238A patent/JPS5755300A/ja active Granted
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3017820U (ja) * | 1994-12-08 | 1995-11-07 | 株式会社大紅 | 車輪に付着した泥土の除去装置 |
Also Published As
Publication number | Publication date |
---|---|
JPS5755300A (en) | 1982-04-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5308024A (en) | Disturbance torque compensated three axis yaw control system | |
US3813067A (en) | Attitude stabilization system | |
US3741500A (en) | A cmg fine attitude control system | |
US4038527A (en) | Simplified strapped down inertial navigation utilizing bang-bang gyro torquing | |
US5205518A (en) | Gyroless yaw control system for a three axis stabilized, zero-momentum spacecraft | |
JPH0319120B2 (en]) | ||
JPH04293698A (ja) | 3軸安定方式の人工衛星のための姿勢制御装置 | |
US5608634A (en) | Low noise spacecraft body rate sensing arrangement for attitude control | |
WO1998016425A9 (en) | Feedback motion compensation for spacecraft payload | |
US5875676A (en) | Non colocated rate sensing for control moment gyroscopes | |
US5115570A (en) | Method for eliminating gyro errors | |
US6471161B1 (en) | Satellite attitude control system | |
US5787368A (en) | Spacecraft yaw control using only wheel speed measurements processed through a simple filter bank | |
JPS6147760B2 (en]) | ||
US6867642B1 (en) | Realtime adaptive notch compensator | |
JP3031216B2 (ja) | 宇宙機搭載用光アンテナの指向角制御装置 | |
US5357817A (en) | Wide bandwidth stable member without angular accelerometers | |
US20050090948A1 (en) | Process for determining the position of a spacecraft with the aid of a directional vector and a total angular momentum measurement | |
US2591938A (en) | Gyroscope control system for dirigible craft | |
US3518771A (en) | North-seeking gyroscope | |
US3540678A (en) | Method of and apparatus for controlling the transverse acceleration and roll damping of steerable aerodynamic bodies | |
EP1134640B1 (en) | Attitude control system for a spacecraft | |
JPH07210202A (ja) | 水中ロボット姿勢制御装置 | |
CA1167669A (en) | Inertial platforms | |
JP2748187B2 (ja) | ジャイロコンパスの誤差修正装置 |