DocumentCode :
2731383
Title :
Deployment and retrieval simulation of a single tether satellite system
Author :
Carter, J. Theron ; Greene, Michael
Author_Institution :
Dept. of Electr. Eng., Auburn Univ., AL, USA
fYear :
1988
fDate :
0-0 1988
Firstpage :
657
Lastpage :
660
Abstract :
The Getaway Tether Experiment (GATE) is a single-tether satellite system for the study of tether dynamics and electrodynamic technology. One goal of GATE is to measure and control tether disturbances such as those induced by micrometeorite impact, using an active reel type deployer that can retrieve and deploy the tether. A computer simulation of the retrieval and deployment characteristics is essential in properly designing a closed-loop controller for the tethered system. A simulation of a single-tether system has been written which allows the tether to be actively reeled in (retrieval) or passively reeled out (deployment) of the mother subsatellite. Simulation results are presented which show the effects of retrieval and deployment on the system. Three cases are considered: exponential retrieval rate, constant retrieval rate, and pulsed deployment.<>
Keywords :
aerospace computing; aerospace control; artificial satellites; digital simulation; GATE; Getaway Tether Experiment; aerospace computing; aerospace control; closed-loop controller; deployment; micrometeorite impact; retrieval simulation; single tether satellite system; Aerodynamics; Artificial satellites; Computational modeling; Computer simulation; Control systems; Electrodynamics; Equations; Lagrangian functions; Potential energy; Springs;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Theory, 1988., Proceedings of the Twentieth Southeastern Symposium on
Conference_Location :
Charlotte, NC, USA
ISSN :
0094-2898
Print_ISBN :
0-8186-0847-1
Type :
conf
DOI :
10.1109/SSST.1988.17130
Filename :
17130
Link To Document :
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