Attitude control for small satellites using control moment gyros

Acta Astronautica

Volumn 51, Issue 1-9, 2002, Pages 101-111

  Lappas, V J ^a   Steyn, W H ^a   Underwood, C I ^a  

^a UNIVERSITY OF SURREY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; AEROSPACE ENGINEERING; ASTRONOMICAL SATELLITES; DATA COMMUNICATION SYSTEMS; RADAR; VECTORS; VELOCITY MEASUREMENT;

ATTITUDE CONTROL SYSTEMS (ACS); CONTROL MOMENTUM GYROS (CMG); MICROSATELLITES; SPACE MISSION;

AIRCRAFT;

EID: 2542447979     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(02)00089-9     Document Type: Conference Paper

References (17)

1. rd International Conf. on Spacecraft Guidance, Navigation and Control Systems, pages 523-528, 1997
2. th International Conf. on Spacecraft Guidance, Navigation and Control Systems, pages 393-398, 2000
3. Blondin, J.C., " Small-CMG's: Needs, Capabilities, Trades and Implementation", AAS/AIAA GNC Rocky-Mountain Conference, 1996
4. Wie, B., "Space Vehicle Dynamics and Control", AIAA Educational Series, Tempe, Arizona 1998
5. Schaub, H., Junkins, J.L., Vadali, S.R., "Feedback control law for variable speed control moment gyros", Journal of the Astronautical Sciences, Vol. 46, No.3, 307-328, 1998
6. Kurokawa, H., Yajima, N., Usui, S., A new steering law of a Single-Gimbal CMG system of a pyramid configuration, IFAC Automatic Control in Space, ACS1985-J, pages 251-257, 1985
7. Schaub, H., Junkins, J.L., "Singularity avoidance using null motion and variable-speed control moment gyros", Journal of Guidance, Control and Dynamics, Vol.23, No. 1, pages 11-16, 2000
8. Wie, B., Bailey, D., Heiberg, C., "Rapid Multi-Target Acquisition and Pointing Control of Agile Spacecraft", AIAA Guidance, Navigation and Control Conference, Denver, Colorado, August 2000
9. Wie, B., Bailey, D., Heiberg, C., "Singularity Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros", Proc. Of the International Symposium on Space Technology and Science, 2000
10. Margulies, G., Auburn, J.N., "Geometric Theory of Single-Gimbal Control Moment Gyro Systems", Journal of the Astronautical Sciences, Vol. XXVI, No. 2, pages 159-191 , 1978
11. Bedrossian, N.S., "Steering law design for redundant single gimbal control moment gyroscopes", MSc. Thesis, MIT, 1987
12. th AIAA/USU Small Satellite Conference proceedings, SSC00-VIII-8, August 2000
13. Steyn, W.H., Hashida Y., "An Attitude Control System for a Low-Cost Earth Observation Satellite with Orbit Maintenance Capability", Proceedings of the 13th Annual AIAA/USU Conference on Small Satellites, Utah State University, Logan, Utah, August 1999
14. Oh, H.S., Vadali, S.R., "Feedback Control and Steering Laws for Spacecraft Using Single Gimbal Control Moment Gyros", The Journal of the Astronautical Sciences, Vol.39, No.2, pages 183-203, 1994
15. Lappas, V.J., Steyn, W.H., Underwood, C.I., "Control Moment Gyro Gimbal Angle Compensation using Magnetic Control During External Disturbances", AIAA Guidance, Navigation and Control Conference ,Montreal, Quebec, Canada, 2001
16. th AIAA/USU Small Satellite Conference, SSC01-I-6, August 2001
17. Lappas, V.J., Steyn, W.H., Underwood, C.I., "Control Moment Gyro Gimbal Angle Compensation using Magnetic Control Under External Disturbances", Electronic Letters, Vol.37, No.9, April 2001