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H2/H control design: LMI techniques for space applications

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5 Author(s)

For ill-conditioned systems, two LMI approaches for the H2 /H design are compared: a first with an optimisation phase, and a second by replacing the optimisation stage by a feasibility one. A lower bound for a generalised H2-norm is proposed. These two techniques are applied to two aerospace applications using a CAD for space systems developed by MMS, called ASTROLAB

Published in:

Control Applications, 1998. Proceedings of the 1998 IEEE International Conference on  (Volume:2 )

Date of Conference:

1-4 Sep 1998