DocumentCode :
551267
Title :
Design of multi-mode flight control system for unmanned helicopter
Author :
Xu Hongzhe ; Huang Jim ; Zhou Yaoming
Author_Institution :
Dept. of Aeronaut. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear :
2011
fDate :
22-24 July 2011
Firstpage :
3660
Lastpage :
3663
Abstract :
Based on the special requirements of flight control and navigation system of unmanned helicopter, this paper present the main framework of flight control system in a certain type of unmanned helicopter, proposed three flight control modes based on different design stages, gave the autonomous control algorithm and the smoothing method while switching between remote control mode and stability augmentation mode, ultimately proved the feasibility of flight control and navigation program through the semi-physical simulation test and flight test.
Keywords :
aerospace robotics; aircraft control; control system synthesis; helicopters; mobile robots; path planning; remotely operated vehicles; stability; telerobotics; autonomous control algorithm; flight test; multimode flight control system design; navigation system; remote control mode; semiphysical simulation test; smoothing method; stability augmentation mode; unmanned helicopter; Aerospace control; Computational modeling; FCC; Helicopters; Servomotors; Switches; Autonomous Control; FCC; Flight Control; Semi-physical Simulation; Stability Augmentation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2011 30th Chinese
Conference_Location :
Yantai
ISSN :
1934-1768
Print_ISBN :
978-1-4577-0677-6
Electronic_ISBN :
1934-1768
Type :
conf
Filename :
6001612
Link To Document :
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