DocumentCode :
2755806
Title :
Modeling and Control for Triadic Compound Controlled Flying Saucer
Author :
Xu, Shenghong ; Wu, Jinhua ; Gu, Wenjin
Author_Institution :
Dept. of Control Eng., Naval Aeronaut. Eng. Acad., Yantai
Volume :
2
fYear :
0
fDate :
0-0 0
Firstpage :
6293
Lastpage :
6297
Abstract :
The flying saucer is an unconventional flying vehicle. The thrust-vectoring/moving-mass compound control system applied to it has good flight control performance, but also has demerits. In order to overcome the demerits, the thrust-vectoring/direct-force/moving-mass triadic compound control system is proposed, and the triadic compound controlled flying saucer is modeled. According to the longitudinal movement assumption, the fuzzy controller and control distribution rule are designed for the pitching angle tracking loop. The simulation results show that the design can take advantage of the compounding superiority of all the control subsystems and has preferable flight control performance
Keywords :
aerospace control; fuzzy control; motion control; angle tracking loop; control distribution rule; direct-force control system; flight control; flying saucer; flying vehicle; fuzzy control; longitudinal movement; moving-mass compound control system; thrust-vectoring control system; triadic compound control; Aerospace control; Aerospace engineering; Aerospace simulation; Control engineering; Control system synthesis; Control systems; Force control; Fuzzy control; Tracking loops; Vehicles; control distribution; flying saucer; fuzzy control; mathematic model; triadic compound control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
Conference_Location :
Dalian
Print_ISBN :
1-4244-0332-4
Type :
conf
DOI :
10.1109/WCICA.2006.1714294
Filename :
1714294
Link To Document :
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