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http://dx.doi.org/10.5139/JKSAS.2005.33.10.051

A Study on Multiple Spacecraft Formation-keeping Control  

No, Tae-Soo (전북대학교 기계항공시스템공학부)
Lee, Jae-Gyu (전북대학교 항공우주공학과 대학원)
Jung, Ok-Chul (한국전자통신연구원)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.33, no.10, 2005 , pp. 51-59 More about this Journal
Abstract
In this paper, results of a multiple spacecraft formation-keeping control using the orbital relative motion and optimization technique are presented. To analyze and predict the relative motion between the formation-flying satellites, a closed-form orbit propagator obtained using the method of ephemeris compression is used. This closed-form orbit propagator is combined with optimization technique to plan a series of impulsive maneuvers, which maintain the formation configuration within the specified limit. As an example, this method is applied to the problem of maintaining the projected circular formation geometry and results from nonlinear simulation are presented.
Keywords
Satellite Formation Flying; Projected Circular Formation Relative Orbit Propagator; Constrained Optimization;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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