A compact CMG product for agile satellites

European Space Agency, (Special Publication) ESA SP

Volumn , Issue 516, 2003, Pages 27-32

  Defendini, Ange ^a   Faucheux, Philippe ^a   Guay, Pascal ^a   Morand, Julien ^a   Heimel, Horst ^b  

^a AIRBUS DEFENCE AND SPACE   (Germany)

^b Teldix GmbH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; ELECTRONIC GUIDANCE SYSTEMS; GYROSCOPES; SPACE FLIGHT; STANDARDS; TORQUE;

AGILE SATELLITES; CONTROL MOMENT GYROSCOPES; GUIDANCE ALGORITHMS;

SATELLITES;

EID: 0038491557     PISSN: 03796566     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

1. "Pleiades HR Satellites: a Solution for Military and Civilian Needs in Metric-Class Optical Observation", P. Damilano, 15th USU Conference on Small Satellites SSC01-I-4, 2001
2. "Performances of the Pléiades-HR Agile Attitude Control System" Bénédicte Girouart, Isabelle Sebbag, Jean-Michel Lachiver, 5th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, Oct. 2002
3. "Low cost CMG-based AOCS designs" A. Defendini, K. Lagadec & all, 4th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, 1999