Optimization of magnetic attitude- and angular momentum control for low earth orbit satellites

European Space Agency, (Special Publication) ESA SP

Volumn , Issue 381, 1997, Pages 559-566

  Bals, J ^a   Fichter, W ^b   Surauer, M ^b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

Magnetic Control; Momentum Bias Satellite; Multi Objective Optimization; Robustness Analysis

Indexed keywords

EID: 5244353898     PISSN: 03796566     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (5)

1. Fisher J. et al. 1995, Magnetic Momentum Bias Attitude Control with Two-Gimballed Appendages, in AAS Guidance and Control Conference. Keystone, USA, February 1995.
2. Fichter W. et al. 1996, Magnetic Attitude- and Angular Momentum Control Design for Bias Momentum Satellites in Low Earth Orbits, in IFAC World Congress, San Francisco, USA, July 1996.
3. ®, in ESA Workshop on Spacecraft Guidance Navigation and Control Systems Software, for Design and Implementation, Noordwijk, Netherlands.
4. Elmqvist H., 1993, Object-Oriented Modeling and Automatic Formula Manipulation in Dymola, in Scandinavian Simulation Society SIMS'93, Kongsberg, Norway. (also see Dymola homepage: http://www.dynasim.se).
5. Enderle et al., 1996, Concept of Attitude Control Simulation of Equator-S using Object Oriented Modeling, in 3rd ESA Conference on Spacecraft Guidance Navigation and Control Systems, Noordwijk, Netherlands, November 1996.