[1]SUN Shihao,JIA Yingmin.Attitude and orbit control of spacecrafts for motion reconstruction of flying around and approaching the tumbling target[J].CAAI Transactions on Intelligent Systems,2016,11(6):818-826.[doi:10.11992/tis.201611022]
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Attitude and orbit control of spacecrafts for motion reconstruction of flying around and approaching the tumbling target
CAAI Transactions on Intelligent Systems[ISSN 1673-4785/CN 23-1538/TP] Volume:
11
Number of periods:
2016 6
Page number:
818-826
Column:
学术论文—智能系统
Public date:
2017-01-20
- Title:
- Attitude and orbit control of spacecrafts for motion reconstruction of flying around and approaching the tumbling target
- Keywords:
- motion reconstruction; similarity; flying around; tumbling; attitude and orbit control; spacecrafts
- CLC:
- TP18;V416.2
- DOI:
- 10.11992/tis.201611022
- Abstract:
- This paper deals with the attitude and orbit control problem for motion reconstruction of spacecrafts flying around and approaching the tumbling target during ground experiments. Firstly, a 6-DOF similarity model is established to describe the integrated attitude and orbit motion, which is suitable for the experimental verification with the practical constraints on the space size, running velocity and time involved. Secondly, the polynomial approach is used to design the motion reference trajectory that can ensure finite-time convergence and good dynamic performances, based on which, an integrated attitude and orbit control law is proposed by the back-stepping method and the corresponding closed-loop stability is proved. Finally, a numerical example is included to illustrate the effectiveness of the obtained results.
- References:
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