Non-minimum phase output reference trajectory tracking for a PVTOL aircraft

被引：8
|
作者：
Sira-Ramírez, W [1 ]
机构：
[1] IPN, CINVESTAV, Dept Ing Elect, Mexico City 07300, DF, Mexico
来源：
PROCEEDINGS OF THE 2000 IEEE INTERNATIONAL CONFERENCE ON CONTROL APPLICATIONS | 2000年
关键词：
D O I：
10.1109/CCA.2000.897544
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
An approximate solution to the general reference trajectory tracking problem, specified in terms of a desired behavior for the non-minimum phase aircraft center of mass position coordinates, is proposed by indirectly defining a suitable trajectory tracking task for the (minimum phase) flat outputs of the system represented by the equivalent to the Huygen's center of oscillation of the aircraft. The approach uses an approximating sequence which appears to be related to an infinite order differential flatness of the system with respect to the non-minimum phase output variables.
引用
收藏
页码：838 / 843
页数：6
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