考虑避障的航天器编队轨道容错控制律设计

doi:10.7527/S1000-6893.2017.321129

Abstract

Abstract:

To solve the flying safety issues of spacecraft formation,including fault tolerance and obstacle/collision avoidance,a novel adaptive translational control method is proposed.Specifically,the proposed method combines the core ideas of artificial potential function guidance and sliding mode control method.A special artificial potential function is designed to encode the collision/obstacle avoidance requirement,and then a coordination controller is presented to enable the spacecraft formation to maintain the predetermined configuration while tracking a target,and to be able to avoid all possible collisions between members in formation or with respect to a non-cooperative obstacle.Furthermore,by introducing adaptive laws into the controller,the robustness of the closed-loop system is further improved in respect to external disturbances,parameter uncertainties and even severe actuator faults.Typical simulations are performed to illustrate the effectiveness of the proposed method.

Key words: spacecraft formation flying control, fault-tolerant control, artificial potential function guidance, obstacle avoidance, collision avoidance

CLC Number:

V412.4⁺1

MA Guangfu, DONG Hongyang, HU Qinglei. Fault-tolerant translational control for spacecraft formation flying with collision avoidance requirement[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(10): 321129-321129.

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Fault-tolerant translational control for spacecraft formation flying with collision avoidance requirement

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