Entry trajectory Optimization for Hypersonic Vehicle based on time-scales separation guidance with Waterweeds algorithm

被引：0

作者：

Liu, Xudong ^{[1
]}

Cheng, Lin ^{[1
]}

Zhang, Qingzhen ^{[1
]}

Jiang, Lingtong ^{[1
]}

机构：

[1] Beihang Univ, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China

来源：

2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2016年

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper focuses on the hypersonic vehicle in consideration of oscillation and aerodynamic heating problems during reentry process, for trajectory optimization, penalty function method and epsilon level comparison are introduced for transforming the unconstrained waterweeds algorithm into constrained algorithm to solve multi-objective optimization problems, in which a novel and more precise criterion based on time-scales separation guidance for oscillation optimization is put forward indicating waterweeds algorithm to get a better optimal result. The algorithm transformed is successfully applied to trajectory design.

引用

页码：209 / 215

页数：7

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