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Analysis of formation flying control of a pair of nano-satellites

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4 Author(s)
Veres, S.M. ; Sch. Eng. Sci., Univ. of Southampton, Highfield, UK ; Gabriel, S.B. ; Rogers, E. ; Mayne, D.Q.

Gives an analysis and provides implementable solutions for constrained control problems of stabilization and maneuver control of two nano-satellites. The methodology provides solutions under various constraints of propulsion and differential drag control: magnitude constraints, disturbances and measurement errors are taken into account. The methods are illustrated in simulation of a realistic nano-satellite pair

Published in:

Decision and Control, 2001. Proceedings of the 40th IEEE Conference on  (Volume:2 )

Date of Conference:

2001