Adaptive Tracking Control of Hypersonic Re-entry Vehicle with Uncertain Parameters

被引：0
|
作者：
Bai, Chen [1 ]
Lian, Chengbin [1 ]
Ren, Zhang [1 ]
Fan, Yao [1 ]
Qi, Peng [2 ]
机构：
[1] Beihang Univ, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
[2] Fourth Acad CASC, Artillery Representat Off 2, Xian, Peoples R China
来源：
2013 THIRD INTERNATIONAL CONFERENCE ON INSTRUMENTATION & MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC) | 2013年
关键词：
hypersonic re-entry vehicle; adaptive control; observers; uncertain parameters;
D O I：
10.1109/IMCCC.2013.354
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The problem of hypersonic re-entry vehicle attitude control with uncertain parameters is addressed. Aimed at a class of affine nonlinear system, adaptive control with observer is proposed. It is proved that observer error of uncertain parameters and tracking error of system output can uniformly asymptotically converge to zero. For implementation on hypersonic re-entry vehicle, two-loop attitude control is designed with aerodynamic derivatives considered as uncertain parameters. Simulations on 6DOF model of HRV show that the proposed adaptive control can keep good tracking performance in case of uncertain parameters.
引用
收藏
页码：1594 / 1597
页数：4
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