TUBE STOCHASTIC OPTIMAL CONTROL FOR NONLINEAR CONSTRAINED TRAJECTORY OPTIMIZATION PROBLEMS

被引:0
|
作者
Ozaki, Naoya [1 ]
Campagnola, Stefano [2 ]
Funase, Ryu [3 ]
机构
[1] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Dept Space Flight Syst, Sagamihara, Kanagawa 2525210, Japan
[2] CALTECH, Jet Prop Lab, Outer Planet Mission Anal Grp, Pasadena, CA 91109 USA
[3] Univ Tokyo, Dept Aeronaut & Astronaut, Bunkyo Ku, 7-3-1 Hongo, Tokyo 1138656, Japan
基金
美国国家航空航天局;
关键词
MODEL-PREDICTIVE CONTROL; UNCERTAINTY; SYSTEMS;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Recent low-thrust space missions have highlighted the importance of designing trajectories that are robust against uncertainties. In its complete form, this process is formulated as a nonlinear constrained stochastic optimal control problem. This problem is among the most complex in control theory, and no practically applicable method to low-thrust trajectory optimization problems has been proposed to date. This paper presents a new algorithm to solve stochastic optimal control problems with nonlinear systems and constraints. The proposed algorithm uses the unscented transform to convert a stochastic optimal control problem into a deterministic problem, which is then solved by trajectory optimization methods such as differential dynamic programming. Two numerical examples, one of which applies the proposed method to low-thrust trajectory design, illustrate that it automatically introduces margins that improve robustness. Finally, Monte Carlo simulations are used to evaluate the robustness and optimality of the solution.
引用
收藏
页码:281 / 300
页数:20
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