Singular perturbation analysis of optimal glide

被引：17

作者：

Shapira, A ^{[1
]}

Ben-Asher, JZ ^{[1
]}

机构：

[1] Technion Israel Inst Technol, Fac Aeronaut Engn, IL-32000 Haifa, Israel

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2004年 / 27卷 / 05期

关键词：

D O I：

10.2514/1.2104

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Open-loop and closed-loop trajectories for maximum range gliders that possess a limited amount of initial energy were analyzed. It was found that open-loop solution showed good agreement with the numerical solution of Singular Perturbation Theory (SPT) in all state variables. It was also found that closed-loop solution produced range that coincided with the numerical optimal solution. The results show that both the solutions are simple and easy to implement.

引用

页码：915 / 918

页数：4

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