Application of Optimizing Control in Determining Flight Range of Aircraft

被引：0

作者：

Wang, Xin ^{[1
]}

Yao, Jun ^{[1
]}

Zhang, Jian ^{[1
]}

机构：

[1] Shenyang Ligong Univ, Shenyang, Peoples R China

来源：

ICIEA 2010: PROCEEDINGS OF THE 5TH IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS, VOL 2 | 2010年

关键词：

optimizing control; maximum principle; flight range; aircraft;

D O I：

暂无

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

For the issue of determination of flight range of controlled aircraft, under the condition of given constrained control, linear differential movement equations of aircraft are chosen and solved in a comparatively short time to determine the flight range based on maximum principle in modern optimizing control theory. The example illustrates that calculation accuracy is high, and the proposed method is effective and feasible and also has reference value for engineering application.

引用

页码：228 / 231

页数：4

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