DocumentCode
538824
Title
Research on UAV Degrade Control System under Sensor Fault State
Author
Zhai, Xiaohua ; Liu, Jian´an ; Qian, Zhengzai ; Xin, Gongcai
Author_Institution
First Aeronaut. Inst. of Air Force, Xinyang, China
Volume
2
fYear
2010
fDate
16-17 Dec. 2010
Firstpage
20
Lastpage
23
Abstract
In the low-cost Unmanned Aerial Vehicle (UAV), in order to ensure the security of the system and reduce costs, degrade control system under the sensor fault state is becoming more and more highly regarded. Degrade control adopted less sensor configuration to achieve the desired control functions. In the low-cost prototype UAV research and development process, degrade control not only can reduce system configuration, lower system cost and, more importantly, the degrade control of the system ensures security of the system under the fault state. Attitude control is the most commonly used mode in UAV, and this paper will focus on designing of degrade control of attitude control loop.
Keywords
aircraft control; attitude control; control system synthesis; mobile robots; remotely operated vehicles; sensors; UAV degrade control system; attitude control loop; sensor fault state; unmanned aerial vehicle; Aircraft; Attitude control; Control systems; Damping; Turning; Unmanned aerial vehicles; Attitude Control; Degrade Control; Fault; Sensor;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Systems (GCIS), 2010 Second WRI Global Congress on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-9247-3
Type
conf
DOI
10.1109/GCIS.2010.189
Filename
5708669
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