Trajectory Optimization for High-Speed and Long-Range Interceptor Based on Improved Adaptive hp Pseudospectral Method

被引:1
|
作者
Luo, Changxin [1 ]
Zhou, Chijun [1 ]
Li, Jiong [1 ]
Lei, Humin [1 ]
机构
[1] AF Engn Univ, Air & Missile Def Coll, Xian 710051, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
MESH REFINEMENT METHOD;
D O I
10.1155/2022/7958272
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The trajectory optimization design of interceptor is very important in the defense combat against a class of high-speed and strong-maneuvering aircraft. At present, an important idea is to use hp pseudospectral method to offline optimizes the trajectory of interceptor, but the solving efficiency of this method needs to be further improved. Aiming at this issue, an improved adaptive hp pseudospectral method is proposed in this paper. In order to shorten the solving time of the algorithm, the proposed method has two main improvements on the basis of the traditional hp pseudospectral method: on one hand, by judging the positions of the control sudden change points, prerefine the mesh around them according to certain rules. On the other hand, the curvature of the system state curve is used as the criterion to segment the original mesh nonuniformly so that more mesh points can be allocated where the curvature is large. These two points together ensure that the collocation point resources can be used more efficiently in the mesh refinement process. The simulation results show that the proposed method can solve the optimized trajectory of interceptor effectively, and it also proves that this method has higher solving efficiency than the traditional adaptive hp method.
引用
收藏
页数:23
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