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