Application of Dynamic Programming Approach to Aircraft Take-Off in a Windshear

被引:4
作者
Botkin, N. D. [1 ]
Turova, V. L. [1 ]
机构
[1] Tech Univ Munich, Ctr Math, Chair Appl Math, D-85748 Garching, Germany
来源
NUMERICAL ANALYSIS AND APPLIED MATHEMATICS (ICNAAM 2012), VOLS A AND B | 2012年 / 1479卷
关键词
Optimal control; State constraints; Hamilton-Jacobi-Bellman-Isaacs equations; Viscosity solutions; Finite difference schemes;
D O I
10.1063/1.4756373
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
Application of dynamic programming method to the problem of aircraft control during take-off in a windshear is considered. A simplified four dimensional model of the aircraft dynamics is used, and stable numerical algorithms for solving Hamilton-Jacobi-Bellman-Isaacs equations arising from differential games with state constraints are utilized for the control design.
引用
收藏
页码:1226 / 1229
页数:4
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