On-line approximation based aircraft longitudinal control

被引：0

作者：

Farrell, J ^{[1
]}

Sharma, M ^{[1
]}

Polycarpou, M ^{[1
]}

机构：

[1] Univ Calif Riverside, Dept Elect Engn, Riverside, CA 92521 USA

来源：

PROCEEDINGS OF THE 2003 AMERICAN CONTROL CONFERENCE, VOLS 1-6 | 2003年

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This document derives stable on-line approximation based control algorithms for application to the longitudinal control (gamma, alpha, Q, V) for an uninhabited combat air vehicle (UCAV). The objectives of the control approach are to stabilize the aircraft dynamics and achieve accurate command tracking in the presence of significant nonlinear model error. This error could be due to decreased modeling effort during the design process or the result of events that occur during the vehicle flight (i.e., battle damage). Lyapunov stability analysis and simulation demonstrations of the achieved performance are included.

引用

页码：1011 / 1019

页数：9

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