Journal of Astronautics

Journal of Astronautics ›› 2017, Vol. 38 ›› Issue (9): 956-963.doi: 10.3873/j.issn.1000-1328.2017.09.008

Previous Articles     Next Articles

Closed Loop Optimal Guidance for Multi Constrained Rendezvous with Angles Only Navigation

LUO Jian jun, LV Dong sheng, GONG Bai chun,YIN Ze yang   

  1. 1. School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China;
    2. Science and Technology on Aerospace Flight Dynamics Laboratory, Xi’an 710072, China;
    3. School of Astronautics,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2017-04-05 Revised:2017-06-26 Online:2017-09-15 Published:2017-09-25

PDF

585

Abstract:

The closed-loop optimal guidance problem of the multi-objective and multi-constrained autonomous rendezvous with angles-only navigation is investigated in this paper. Firstly, considering the observability and robustness requirements, the performance indexes of the multi-objective optimization of the angles-only navigation and rendezvous guidance are established. On this basis, the objective function of the multi-objective and multi-constrained optimal rendezvous problem, and the solution method of the optimal guidance problem based on convex optimization are presented. Secondly, the framework and solution of the closed-loop angles-only navigation and guidance are proposed according to the “coupling” relationship between the navigation and guidance. Finally, the effect of the observability on the navigation and guidance performance is analyzed by simulation, and the effectiveness of the proposed method is verified.

Key words: Observability, Multiple constraints, Robustness, Convex optimization, Closed loop guidance

CLC Number: