Title :
The design of flight control law based on integral separation PID algorithm
Author :
Du Wei-Yang ; Zhong-Zhou, Jian ; Chen, Tian-xiang
Author_Institution :
First Aeronaut. Inst. of Air Force, Xinyang, China
Abstract :
The quality of flight control law design is to ensure that an important prerequisite for normal flight the aircraft, This article case of an aircraft, which based on the choice of flight control law, design and implementation of a relatively independent channel flight control law, get a better flight control mode in the simulation.
Keywords :
aircraft control; control system synthesis; three-term control; aircraft normal flight; integral separation PID algorithm; relatively independent channel flight control law design; Aerospace control; Aircraft; Reliability; Switches; Tracking loops; Flight control system; PID algorithm; flight control law;
Conference_Titel :
Electronics and Optoelectronics (ICEOE), 2011 International Conference on
Conference_Location :
Dalian, Liaoning
Print_ISBN :
978-1-61284-275-2
DOI :
10.1109/ICEOE.2011.6013278
