Fully magnetic attitude control subsystem for picosat platforms

Author:

Colagrossi Andrea,Lavagna Michèle

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference22 articles.

1. Acquisition of a desired pure-spin condition for a magnetically actuated spacecraft;Avanzini;Journal of Guidance, Control, and Dynamics,2013

2. Magnetic detumbling of a rigid spacecraft;Avanzini;J. Guid. Control Dyn.,2012

3. Fundamentals of Astrodynamics;Bate,1971

4. Bhat, S.P., Dham, A.S., 2003. Controllability of spacecraft attitude under magnetic actuation. In: 42nd IEEE Conference on Decision and Control, 2003, vol. 3, pp. 2383–2388.

5. Colagrossi, A., Bucci, L., Lavagna, M., Parissenti, G., 2016. GNC design and testing for an IOD/IOV 1/3U platform. Presentation presented at the 8th European CubeSat Symposium: Nanosatellites for Science and Technology, September 2016, London, UK.

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