Hypersonic Boost Glide Vehicle Trajectory Optimization Using Genetic Algorithm

被引:25
作者
Kumar, G. Naresh [1 ]
Penchalaiah, D. [2 ]
Sarkar, A. K. [1 ]
Talole, S. E. [3 ]
机构
[1] DRDL, Directorate Syst, Hyderabad, India
[2] Directorate Syst, Hyderabad, India
[3] DIAT, Dept Aerosp Engn, Pune, Maharashtra, India
关键词
Controllability; Genetic algorithms (GA)s; Hypersonic boost glide vehicle; Trajectory optimization;
D O I
10.1016/j.ifacol.2018.05.020
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Trajectory optimization formulation for hypersonic boost glide class of vehicle to achieve maximum range under various in-flight and impact constraints is proposed. The formulation considers vehicle controllability using aerodynamic forces also as one of the path constraint by imposing a constraint on maximum altitude. Genetic algorithm is used to solve the dynamic optimization problem and a trajectory for maximum range has been generated with all the in-flight and terminal constraints. The results bring out the effectiveness of genetic algorithm in providing feasible solution to the proposed problem. Superiority of the approach over gradient based method in terms of range and simplicity in formulating complex in-flight constraints is also demonstrated. (C) 2018, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
引用
收藏
页码:118 / 123
页数:6
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