Solar sail hybrid trajectory optimization for non-Keplerian orbit transfers

被引：32

作者：

Hughes, GW ^{[1
]}

McInnes, CR ^{[1
]}

机构：

[1] Univ Glasgow, Dept Aerosp Engn, Glasgow G12 8QQ, Lanark, Scotland

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2002年 / 25卷 / 03期

关键词：

Computational methods - Convergence of numerical methods - Estimation - Genetic algorithms - Optimization - Orbits - Position control - Solar energy;

D O I：

10.2514/2.4924

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A trajectory optimization tool was developed which hybridized a genetic algorithm (GA) with sequential quadratic programming (SQP). When applied to the difficult problem of preliminary mission planning for high-performance solar sail transfers to displaced non-Keplerian orbits (NKOs), it appeared to identify near-optimal trajectories with relative ease. A small number of segments reduced the computational burden imposed by using a GA.

引用

页码：602 / 604

页数：3

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