Toward improvement of tracking performance - nonlinear feedback for linear systems

被引:300
作者
Lin, ZL [1 ]
Pachter, M
Banda, S
机构
[1] Univ Virginia, Dept Elect Engn, Charlottesville, VA 22903 USA
[2] Penn State Univ, University Pk, PA 16802 USA
[3] USAF, Dept Elect & Comp Sci, Wright Patterson AFB, OH 45433 USA
[4] USAF, Wright Lab, Flight Dynam Dir WL FGIC, Wright Patterson AFB, OH 45433 USA
关键词
D O I
10.1080/002071798222433
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 [计算机科学与技术];
摘要
A composite nonlinear feedback tracking control law based on a nominal linear controller is proposed. The design yields nonlinear feedback laws that both increase the speed of the closed-loop system response to the command input and reduce the overshoot, while not imperilling the small signal performance achieved by the nominal linear feedback controller in the face of actuator amplitude saturation. A modern flight control application is used to demonstrate the effectiveness of the design.
引用
收藏
页码:1 / 11
页数:11
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