Dynamics of an autonomous spacecraft control system at initial transition to a tracking mode
Keyword(s):
The problems of autonomous digital control of the information satellites and space robots during their initial transition to a tracking mode, namely in the initial orientation modes, are considered. Autonomous angular guidance and modularly limited vector digital control using a vector of the modified Rodrigues parameters are applying to bring the spacecraft’s orientation from completely arbitrary to the required one. The developed methods, algorithms and simulation results for a mini-satellite in a sun-synchronous orbit are presented.
2016 ◽
Vol 48
(12)
◽
pp. 27-36
2016 ◽
Vol 11
(1)
◽
pp. 21-33
Multi-layer controller with state-constraint: Vehicle lateral stability control based on fuzzy logic
2021 ◽
pp. 095440702110142