DocumentCode :
2756625
Title :
Time Optimal Tracking Control Approach for Suspended Gravity Compensation System
Author :
Yao, Yansheng ; Mei, Tao ; Sun, Lei ; Zhang, Tao
Author_Institution :
Inst. of Intelligent Machines, Chinese Acad. of Sci., Hefei
Volume :
2
fYear :
0
fDate :
0-0 0
Firstpage :
6493
Lastpage :
6497
Abstract :
A suspension system for studying the dynamic characteristics of space robots working under microgravity condition is introduced. The system can apply a constant force against the gravity of an operating target. The support point on system\´s end-effector synchronously tracking the motion of suspension object is expected to obtain long-time zero-gravity of the target satellite. According to dynamic model of suspension module, a "bang-bang" time-optimal programming which is a human simulated conception, and a precision tracking approach through coarse and precise periods is proposed. The control result is presented and verified by using numerical computation and simulation
Keywords :
aerospace robotics; aerospace simulation; compensation; end effectors; mathematical programming; motion control; time optimal control; tracking; bang-bang time-optimal programming; human-simulated intelligent control; microgravity; precision tracking; space robots; suspended gravity compensation system; suspension system; time optimization; tracking control; Computational modeling; Control systems; Dynamic programming; Gravity; Humans; Numerical simulation; Optimal control; Orbital robotics; Satellites; Target tracking; dynamics; human-simulated intelligent control; simulation; suspension system; time optimization; tracking control approach;
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.2006.1714336
Filename :
1714336
Link To Document :
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