Large-scale direct optimal control applied to a re-entry problem

被引：11

作者：

Bonnans, JF ^{[1
]}

Launay, G ^{[1
]}

机构：

[1] Inst Natl Rech Informat & Automat, Projet PROMATH, F-78153 Rocquencourt, France

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1998年 / 21卷 / 06期

关键词：

D O I：

10.2514/2.4337

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

We present the numerical solution of an atmospheric re-entry problem for the Space Shuttle. We discretize the control and state with identical grid and use a large-scale successive quadratic programming technique. With the help of sliding horizon and successive refinement of the discretization, we can solve on a workstation a problem with 1600 grid intervals, an unusually large figure for this kind of real-world optimal control problem.

引用

页码：996 / 1000

页数：5

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