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Dynamic-measurement modeling of attitude motion for N-bodies spacecraft with applications
KTH, School of Computer Science and Communication (CSC), Theoretical Computer Science, TCS.ORCID iD: 0000-0002-9706-5008
2011 (English)In: Proceedings of the 30th Chinese Control Conference, 2011, 1453-1458 p.Conference paper (Refereed)
Abstract [en]

Modeling analysis technique is one of the most important means in processing spaceflight mission. In this paper, the graph based description is given, and a series of dynamic-measurement system models are built for the attitude motion of a N-bodies spacecraft, which include the states evolvement equation of the main body, the states evolvement equations of the accessories, the inertia based measurement equations and the celestial bodies based measurement equation and the GPS based measurement equations of attitudes of the N-bodies etc.. These models are educed with some typical methods of theoretical analysis and dynamic description and are simplified into linearized discrete equations. At the end of the paper some valuable applications are pointed out.

Place, publisher, year, edition, pages
2011. 1453-1458 p.
, Proceedings of the 30th Chinese Control Conference, CCC 2011
Keyword [en]
Attitude Motion, Dynamic-Measurement System, N-body Spacecraft, Attitude motions, Celestial bodies, Discrete equations, Graph-based, Measurement equations, Modeling analysis, System models, Dynamic analysis, Measurements, Space flight, Spacecraft, Equations of state
National Category
Control Engineering
URN: urn:nbn:se:kth:diva-150749ISI: 000312652101101ScopusID: 2-s2.0-80053066896ISBN: 9789881725592OAI: diva2:745028
30th Chinese Control Conference, CCC 2011, 22 July 2011 through 24 July 2011, Yantai

QC 20140909

Available from: 2014-09-09 Created: 2014-09-09 Last updated: 2014-09-09Bibliographically approved

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Meinke, Karl
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