Smooth Interpolation-Based Fixed-Final-Time Command Generation

被引：4

作者：

Hong, Haichao ^{[1
]}

Maity, Arnab ^{[2
]}

Holzapfel, Florian ^{[3
]}

Tang, Shengjing ^{[1
]}

Wang, Mengmeng ^{[4
]}

机构：

[1] Beijing Inst Technol, Beijing 100081, Peoples R China

[2] Indian Inst Technol, Mumbai 400076, Maharashtra, India

[3] Tech Univ Munich, D-80333 Munich, Germany

[4] Beihang Univ, Beijing 100083, Peoples R China

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2019年 / 55卷 / 06期

基金：

中国国家自然科学基金;

关键词：

Interpolation; Programming; Missiles; Predictive models; Task analysis; Moon; Jacobian matrices; Generalized model predictive static programming (G-MPSP); missile guidance; smooth interpolation; soft lunar landing; TRAJECTORY OPTIMIZATION; GUIDANCE; ANGLE;

D O I：

10.1109/TAES.2019.2897038

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper proposes a command generation approach based on the smooth interpolation without twist constraints and the input-output relation developed by the generalized model predictive static programming. Commands are efficiently generated to achieve the desired terminal condition at a specified final time in an interpolative manner featuring a noniterative nature. The effectiveness of this approach is demonstrated through three different simulation studies including a double integrator benchmark, a soft lunar landing problem, and a cluster missile guidance problem.

引用

页码：3039 / 3049

页数：11

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