DocumentCode
2109902
Title
A ground docking test facility for docking mechanism
Author
Zhigang, Chen ; Guangyu, Zhang ; Xuezeng, Zhao
Author_Institution
Harbin Inst. of Technol., China
Volume
4
fYear
2004
fDate
13-13 March 2004
Firstpage
2757
Abstract
Chinese space program require extensive testing to verify design and performance and to qualify hardware. For this purpose a docking test facility (DTF) is being designed. It allows reproduction on the ground of the same relative motion and contact forces and torque of two docking mechanisms that would occur in space docking to verify capturing and buffering capabilities of docking mechanism. The DTF can realize five-degree-of-freedom motion with a three-degree-of-freedom turntable and a two-degree-of-freedom carriage. The technique involves gravity balance equipment to eliminate gravitation on the active docking ring, special mass and inertia simulator to simulate spacecraft´s mass and inertia properties, friction compensation using DC servomotor, and momentum compensation using flywheel. This paper describes DTF with emphasis on the configuration, features and functions.
Keywords
aerospace control; aerospace test facilities; flywheels; friction; ground support equipment; servomotors; space vehicles; Chinese space program; DC servomotor; active docking ring; degree of freedom motion; docking mechanism; flywheel; friction compensation; gravity balance equipment; ground docking test facility; inertia properties; momentum compensation; space docking; spacecraft mass; Damping; Delta modulation; Force control; Hardware; Space stations; Space technology; Space vehicles; System testing; Test facilities; Weight control;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1368073
Filename
1368073
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