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Constrained Trajectory Generation for Microsatellite Formation Flying
Abstract Station keeping and reorientation control …
Station keeping and reorientation control of a cluster of fully-actuated low-thrust micro-satellites is considered in this paper. We address the control problem by taking advantage of the fully-actuated structure of the micro-satellite. We propose a very general open-loop solution by solving in real-time constrained trajectory generation problems for stationkeeping and reorientation. Performance of this methodology is reported for a typical micro-satellite format ion flying space mission using the Nonlinear Trajectory Generation software package.
ar Trajectory Generation software package.  +
Authors Mark B. Milam, Nicolas Petit and Richard M. Murray  +
ID 2001b  +
Source Submitted, 2001 AIAA Guidance, Navigation and Control Conference  +
Tag mpm01-gnc  +
Title Constrained Trajectory Generation for Microsatellite Formation Flying +
Type Conference Paper  +
Categories Papers
Modification date
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15 May 2016 06:19:19  +
URL
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http://www.cds.caltech.edu/~murray/preprints/mpm01-gnc.pdf  +
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Constrained Trajectory Generation for Microsatellite Formation Flying + Title
 

 

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