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Thrust Vector Control Algorithm Design for the Cassini Spacecraft

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dc.contributor.author Enright, Paul J. en_US
dc.date.accessioned 2004-10-06T01:27:52Z
dc.date.available 2004-10-06T01:27:52Z
dc.date.issued 1993-02-17 en_US
dc.identifier.citation Irvine, California, USA en_US
dc.identifier.clearanceno 93-0360 en_US
dc.identifier.uri http://hdl.handle.net/2014/34920
dc.description.abstract A preliminary design of the Cassini Thrust Vector Control algorithm which controls the spacecraft attitude during main engine burns is described. The discussion includes software architecture, sensor/actuator characteristics, and vehicle dynamics, as well as controller design and margin analysis via clasical methods, and performance evaluation via simulation. en_US
dc.format.extent 862068 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Algorithm Cassini Thrust Vector Control en_US
dc.title Thrust Vector Control Algorithm Design for the Cassini Spacecraft en_US


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