Cooperative control structures and methods for satellite spin axis control
作者： Richard A. Fowell , Qinghong W. Wang
DOI:
关键词:
摘要: Structures and methods are provided to effect satellite maneuvers in the presence of disturbance torques with enhanced fuel efficiency. A thruster control loop is combined a wheel which wheels respond an estimate (e.g., angular acceleration estimate, torque command or filtered command) create counteracting gyroscopic torque. Simulations invention's have shown they authority all-thruster systems efficiency that rivals all-wheel systems.
lens.org 参考文章(14)
Jeremiah O. Salvatore, Spin stabilization via momentum wheels or similar devices ,(1989)
Santosh Ratan, Neil Evan Goodzeit, Adaptive harmonic disturbance compensation system ,(1996)
Guidance and Control--II American Institute of Aeronautics and Astronautics. ,(1964) , 10.2514/4.864872
Jason Mccanna, Dynamic Imbalance Would Counter Offcenter Thrust ,(1994)
KENNETH R. LORELL, BENJAMIN O. LANGE, An Automatic Mass-Trim System for Spinning Spacecraft AIAA Journal. ,vol. 10, pp. 1012- 1015 ,(1972) , 10.2514/3.50286
Loren I. Slafer, Sibnath Basuthakur, On-board three-axes attitude determination and control system ,(1992)
David S. Uetrecht, Attitude control system for momentum-biased spacecraft ,(1991)
Kenneth R. Lorell, James P. Murphy, All sky pointing attitude control system ,(1973)
Wilhelm Goschel, Method and apparatus for controlling a satellite ,(1979)
Neil E. Goodzeit, Michael A. Paluszek, Low noise spacecraft body rate sensing arrangement for attitude control ,(1992)