The space net is a novel and effective approach in solving the spacecraft capturing problem. In this chapter, the attitude control problem of parent satellite is addressed. At first, the disturbance imposed on the parent satellite is analyzed, and the dynamic process of mass ejection is investigated. In addition, the main factors that affect the performance of the net are analyzed, and based on which, the model of the disturbance torque is developed. At the end of this chapter, the numerical simulations are implemented, and the corresponding results validate the effectiveness of the proposed algorithm.
Attitude Disturbance and Control of Satellite During Space Net Projecting
Lect. Notes Electrical Eng.
Unifying Electrical Engineering and Electronics Engineering ; Chapter : 211 ; 1931-1939
2013-06-15
9 pages
Article/Chapter (Book)
Electronic Resource
English
Improved satellite attitude control using a disturbance compensator
Online Contents | 2004
|British Library Conference Proceedings | 2012
|Satellite attitude control flywheel pair, satellite attitude control system and satellite
European Patent Office | 2020
|