DocumentCode :
466560
Title :
Optimal Trajectory Planning and Control for the Manned Maneuvering Unit
Author :
Yuyang, Wang ; Chun, Sun Fu ; Bin, Xu ; Kun, Zhang Chao
Author_Institution :
Dept. of Comput. Sci. & Technol., Tsinghua Univ., Beijing
Volume :
1
fYear :
2006
fDate :
4-6 Oct. 2006
Firstpage :
763
Lastpage :
769
Abstract :
The optimal trajectories for the manned maneuvering unit (MMU) rescuing disabled crewmembers or equipments in the vicinity of the space station is discussed in this paper, using Clohessy-Wiltshire equations considering integrated influences of several aspects such as minimum fuel, terminal accuracy and time constrains. The targeting errors induced by navigation error and control error are analyzed and poles of C-W equations are illuminated here. Multi-impulse Hill guidance is developed so that highly accuracy rate of the rendezvous can be reached as well as the purpose of energy saving
Keywords :
aerospace control; motion control; optimal control; position control; Clohessy-Wiltshire equations; manned maneuvering unit control; multiimpulse Hill guidance; optimal trajectory planning; rescue trajectory; space station; Equations; Error analysis; Error correction; Optimal control; Process control; Satellite ground stations; Sections; Space stations; Systems engineering and theory; Trajectory; Clohessy-Wiltshire equations; Manned Maneuvering Unit (MMU); Rescue trajectory; Targeting error;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Engineering in Systems Applications, IMACS Multiconference on
Conference_Location :
Beijing
Print_ISBN :
7-302-13922-9
Electronic_ISBN :
7-900718-14-1
Type :
conf
DOI :
10.1109/CESA.2006.4281754
Filename :
4281754
Link To Document :
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