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Space Flyaround and In-orbit Inspection Coupled Control Based on Dual Numbers

Published online by Cambridge University Press:  03 May 2018

Lijun Zhang ,
Hanqiu Li ,
Jianping Liu ,
Shan Qian ,
Yi Lu  and
Hengnian Li
Lijun Zhang*
Affiliation:
(China Xi'an Satellite Control Center, Xi'an, China) (State Key Laboratory of Astronautic Dynamics, Xi'an, China) (State Key Laboratory of Geo-information Engineering, Xi'an, China)
Hanqiu Li
Affiliation:
(China Xi'an Satellite Control Center, Xi'an, China)
Jianping Liu
Affiliation:
(China Xi'an Satellite Control Center, Xi'an, China) (State Key Laboratory of Astronautic Dynamics, Xi'an, China)
Shan Qian
Affiliation:
(China Xi'an Satellite Control Center, Xi'an, China) (State Key Laboratory of Astronautic Dynamics, Xi'an, China)
Yi Lu
Affiliation:
(China Xi'an Satellite Control Center, Xi'an, China) (State Key Laboratory of Astronautic Dynamics, Xi'an, China)
Hengnian Li
Affiliation:
(China Xi'an Satellite Control Center, Xi'an, China) (State Key Laboratory of Astronautic Dynamics, Xi'an, China)
*
(E-mail: alijun_007@163.com)
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Abstract

In this paper, both the proportional derivative feedback control and variable-structure sliding mode control approaches based on dual numbers are presented to design space flyaround and in-orbit inspection missions. Dual-number-based spacecraft kinematics and dynamics models are formulated. The integrated translational and rotational motions can be described in one compact expression, and the mutual coupling effect can be considered. A space flyaround and in-orbit inspection mission model based on dual numbers is derived. Both proportional derivative feedback control and variable-structure sliding mode control laws are designed using dual numbers. Simulation results indicate that both the proposed control system can provide high-precision control for relative position and attitude. Of the two systems, the variable-structure sliding mode control system performs the best.

Keywords

Space flyaroundIn-orbit inspectionDual numbersVariable-Structure sliding mode control
Type
Research Article
Information
The Journal of Navigation , Volume 71 , Issue 5 , September 2018 , pp. 1088 - 1110
Copyright
Copyright © The Royal Institute of Navigation 2018 

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References

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