A different look at output tracking: Control of a VTOL aircraft

被引:216
作者
Martin, P
Devasia, S
Paden, B
机构
[1] UNIV UTAH,MEB,DEPT MECH ENGN,SALT LAKE CITY,UT 84112
[2] UNIV CALIF SANTA BARBARA,CTR CONTROL ENGN & COMPUTAT,ECE DEPT,SANTA BARBARA,CA 93106
[3] UNIV CALIF SANTA BARBARA,DEPT ENGN MECH,SANTA BARBARA,CA 93106
基金
美国国家科学基金会;
关键词
nonlinear theory; inversion; output tracking; aircraft control;
D O I
10.1016/0005-1098(95)00099-2
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper we propose a scheme for output tracking of nonminimum phase Aat systems. The technique, which is applicable even in the minimum phase case, uses an inverse trajectory for feedforward which is stabilized by a state tracker built using the hat output. In contrast to approximate-linearization based control [Hauser, J., S. Sastry and G. Meyer (1992). Nonlinear control design for slightly nonminimum phase systems: application to v/stol aircraft. Automatica, 28, 665-679], which yields good performance in slightly nonminimum phase systems, our approach applies equally well to slightly and strongly nonminimum phase systems. The proposed control scheme and the approximate-linearization based controller are applied to a Vertical Take Off and Landing (VTOL) aircraft example and the performances are compared.
引用
收藏
页码:101 / 107
页数:7
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