|
|
|
|
Adaptive neural network dynamic inversion with prescribed performance for aircraft flight control
|
|
|
|
|
|
|
|
نویسنده
|
gai w. ,wang h. ,zhang j. ,li y.
|
|
منبع
|
journal of applied mathematics - 2013 - دوره : 2013 - شماره : 0
|
|
چکیده
|
An adaptive neural network dynamic inversion with prescribed performance method is proposed for aircraft flight control. the aircraft nonlinear attitude angle model is analyzed. and we propose a new attitude angle controller design method based on prescribed performance which describes the convergence rate and overshoot of the tracking error. then the model error is compensated by the adaptive neural network. subsequently,the system stability is analyzed in detail. finally,the proposed method is applied to the aircraft attitude tracking control system. the nonlinear simulation demonstrates that this method can guarantee the stability and tracking performance in the transient and steady behavior. © 2013 wendong gai et al.
|
|
|
|
|
آدرس
|
college of information and electrical engineering,shandong university of science and technology,qingdao 266590,china,science and technology on aircraft control laboratory,beihang university, China, science and technology on aircraft control laboratory,beihang university, China, college of information and electrical engineering,shandong university of science and technology, China, college of information and electrical engineering,shandong university of science and technology, China
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Authors
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|