DocumentCode
551824
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
Volume
2
fYear
2011
fDate
29-31 July 2011
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Electronics and Optoelectronics (ICEOE), 2011 International Conference on
Conference_Location
Dalian, Liaoning
Print_ISBN
978-1-61284-275-2
Type
conf
DOI
10.1109/ICEOE.2011.6013278
Filename
6013278
Link To Document