Abstract
An improved constrained (IC) steering law for single gimbal control moment gyros (SGCMGs) with deformed pyramid configuration (DPC) is proposed. First of all, the original system with five pyramid configuration (FPC) whose two adjacent gyros are in failure state is reconfigured as a degraded system with DPC. Then, the singular angular momentum hypersurfaces of the original and the degraded systems are plotted via the singular angular momentum equation of SGCMGs. Based on singular surfaces, the differences between FPC and DPC in singularity and momentum envelope are obtained directly, which provide an important reference for steering law design of DPC. Finally, an IC steering law is designed and applied to DPC. The simulation results demonstrate that the IC steering law has advantages in simplicity of calculation, avoidance of singularity and exactness of output torque, which endow the degraded system with fine controllability in a restricted workspace.
Similar content being viewed by others
References
Zhang J.J., Li J.S., Wu H.X.: Study on singularity analysis of large spacecraft SGCMG system. Chin. Space Sci. Technol. 3, 36–41 (2001) (in Chinese)
Wu Z., Wu H.X.: SGCMG system and its steering of the Mir space station. Aerosp. Control 2, 76–80 (1999) (in Chinese)
Pastena M.: Robust control of the smart microsatellite attitude dynamics. Acta Astronaut. 47(2–9), 119–128 (2000)
Kurokawa, H.: A geometric study of single gimbal control moment gyros. Technical Report of Mechanical Engineering Laboratory, Japan, No. 175 (1997)
Montfort, E., Dulot, J.L.: AOCS with magnetic bearing CMG: from failure to recovery. In: Proceedings of the 5th International ESA Conference on Spacecraft Guidance, Navigation and Control Systems, pp. 591–594 (2003)
Tang, L.: A Research on attitude dynamics and control of spacecraft with control moment gyros. (Ph. D. Dissertation), School of Astronautics, Beijing University of Aeronautics and Astronautics (2005) (in Chinese)
Zhang J.R., Rachid A., Zhang Y.: Attitude control for part actuator failure of agile small satellite. Acta Mech. Sin. 24(4), 463–468 (2008)
Kurokawa H.: Constrained steering law of pyramid-type control moment gyros and ground tests. J. Guid. Control Dyn. 20(3), 445–449 (1997)
Margulies G., Aubrun J.N.: Geometric theory of single-gimbal control moment gyro systems. J. Astronaut. Sci. 26(2), 159–191 (1976)
Kurokawa, H.: Exact singularity avoidance control of the pyramid type CMG system. AIAA-94-3559-CP (1994)
Author information
Authors and Affiliations
Corresponding author
Additional information
The project supported by the National Natural Science Foundation of China (10372011).
Rights and permissions
About this article
Cite this article
Jin, L., Xu, S. An improved constrained steering law for SGCMGs with DPC. Acta Mech Sin 25, 713–720 (2009). https://doi.org/10.1007/s10409-009-0269-z
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s10409-009-0269-z