Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach
This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is captured by a service spacecraft. The optimal controller of fully-actuated system is proposed to realize the attitude and orbit stabilization...
Saved in:
Published in | Journal of systems science and complexity Vol. 35; no. 2; pp. 623 - 640 |
---|---|
Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Beijing
Academy of Mathematics and Systems Science, Chinese Academy of Sciences
01.04.2022
Springer Nature B.V |
Subjects | |
Online Access | Get full text |
Cover
Loading…
Be the first to leave a comment!