TRAJECTORY TRACKING CONTROL OF A PVTOL AIRCRAFT BASED ON LINEAR ALGEBRA THEORY

被引：20
|
作者：
Gandolfo, D. [1 ]
Rosales, C. [1 ]
Patino, D. [1 ]
Scaglia, G. [2 ]
Jordan, M. [3 ]
机构：
[1] Univ Nacl San Juan, Inst Automat, San Juan, Argentina
[2] Univ Nacl San Juan, Inst Ingn Quim, San Juan, Argentina
[3] UNS Inst Argentino Oceanog IADO CONICET, Dept Ingn Elect & Comp, Bahia Blanca, Buenos Aires, Argentina
来源：
ASIAN JOURNAL OF CONTROL | 2014年 / 16卷 / 06期
关键词：
PVTOL aircraft; Markov propriety; linear algebra based controller; internal states; tracking error; GLOBAL STABILIZATION; CONTROL DESIGN; VTOL AIRCRAFT; SYSTEMS;
D O I：
10.1002/asjc.819
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 work, a trajectory tracking control design is proposed for the planar vertical takeoff and landing (PVTOL) aircraft using linear algebra theory. The resulting control law is implemented easily since the equation to be solved is not complex. The tracking is achieved providing convergence of the tracking errors to zero, and simulation results show the good performance of the proposed controller.
引用
收藏
页码：1849 / 1858
页数：10
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