Free Final-Time Low Thrust Trajectory Optimization Using Homotopy Approach

被引:3
作者
Lee, Jinsung [1 ]
Ahn, Jaemyung [1 ]
机构
[1] Korea Adv Inst Sci & Technol, Dept Aerosp Engn, Daejeon, South Korea
关键词
Low-thrust trajectory optimization; Homotopic approach; Two-point boundary value problem; PRIMER VECTOR; TECHNOLOGY;
D O I
10.1007/s42405-023-00602-7
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper discusses the application of the homotopy approach to optimizing the free-flight-time low-thrust trajectory considering the performance characteristics. The trajectory optimization problem is formulated as an optimal control problem (two-point boundary value problem). The developed homotopy algorithm to solve the optimal control problem comprises three steps-orbital energy/acceleration matching, flight-time matching, and orbital reshaping. A comprehensive case study demonstrates the effectiveness of the proposed homotopy-based optimization algorithm for an optimal design of a low-thrust trajectory involving long mission time.
引用
收藏
页码:1363 / 1374
页数:12
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