Integration planning of gimbal angle and attitude motion for zero propellant maneuver under attitude and control moment gyroscope constraints

Author:

Wang ZhuoORCID,Xu Rui,Zhu ShengyingORCID,Jiang HuipingORCID,Li Zhaoyu,Liang Zixuan,Luo Da

Funder

National Natural Science Foundation of China

National Key R&D Program of China

Industrial Technology Development Program

Civil Aerospace Technology Research Project of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. An industrial information integration approach to in-orbit spacecraft;Du;Enterprise Inf. Syst.,2016

2. Satellite recovery control strategy based on attitude error information fusion;Du,2007

3. Zero-propellant maneuver guidance;Bedrossian;Control Syst. IEEE,2009

4. Singularity and steering logic for control moment gyros on flexible space structures;Hu;Acta Astronaut.,2017

5. First ever flight demonstration of zero propellant maneuver(TM) attitute control concept;Bedrossian,2007

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