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Autonomous Reorientation of a Manuever-Limited Spacecraft Under Simple Pointing Constraints
Abstract This report presents techniques for using …
This report presents techniques for using discrete finite rotations to reorient a spacecraft from a given initial attitude to a final attitude which satisfies a specified aiming objective. The objective may be a fully specified final orientation or it may require that the spacecraft direct an instrument along a certain direction. Constraints are also imposed on the allowable intermediate orientations that the spacecraft may assume during the course of the maneuver, representing the operational requirements of onboard instrumentation. The algorithms presented consider solutions that will achieve the desired objective with only one or two slew maneuvers, although they may be easily extended to consider more complicated solutions requiring additional maneuvers.
solutions requiring additional maneuvers.  +
Authors Charles A. Vannelli  +
Flags NoRequest  +
ID 1997  +
Source Engineer's Thesis, Caltech, May 1997  +
Tag cav97-eng  +
Title Autonomous Reorientation of a Manuever-Limited Spacecraft Under Simple Pointing Constraints +
Type Thesis  +
Categories Papers
Modification date
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15 May 2016 06:20:06  +
URL
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http://www.cds.caltech.edu/~murray/preprints/cav97-eng.pdf.gz  +
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Autonomous Reorientation of a Manuever-Limited Spacecraft Under Simple Pointing Constraints + Title
 

 

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