DocumentCode
2969128
Title
Time-varying LQ control for autonomous soft landing of small-scale helicopter
Author
Xia Xiaohu ; Zhu Min ; Zhang Xiaotao ; Ge Yunjian
Author_Institution
Inst. of Intell. Machines, Chinese Acad. of Sci., Hefei, China
fYear
2009
fDate
22-24 June 2009
Firstpage
224
Lastpage
227
Abstract
This paper addresses soft landing of miniature helicopter issue and suggests an optimal strategy with appropriate design parameters for a typical soft landing. The time-varying gains and time-varying quadratic performance index LQ control for autonomous soft landing of miniature helicopter examines and simulate. Simulation results have proved that the designed controller is suitable.
Keywords
helicopters; linear quadratic control; mobile robots; remotely operated vehicles; time-varying systems; autonomous soft landing; miniature helicopter soft landing; small-scale helicopter; time-varying LQ control; time-varying gains; time-varying quadratic performance index; Design automation; Feedback; Helicopters; Intelligent sensors; Machine intelligence; Mathematical model; Moon; Optimal control; Performance analysis; Performance gain; Optimal control; linear-quadratic control; quadratic performance index; time-varying;
fLanguage
English
Publisher
ieee
Conference_Titel
Information and Automation, 2009. ICIA '09. International Conference on
Conference_Location
Zhuhai, Macau
Print_ISBN
978-1-4244-3607-1
Electronic_ISBN
978-1-4244-3608-8
Type
conf
DOI
10.1109/ICINFA.2009.5204925
Filename
5204925
Link To Document