Multi-objective H2/H∞/Impulse-to-Peak Control of a Space Launch Vehicle

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Multi-objective H2/H∞/Impulse-to-Peak Control of a Space Launch Vehicle

A multi-objective synthesis problem involvingH2, H∞ and impulse-to-peak performances is investigated. In general, multi-objective control problems are hard problems to solve and do not have exact solutions. Here, an LMI formulation is proposed for the mixedH2/impulseto-peak optimization under an H∞ constraint for LTI discrete-time systems. This framework is then used to control the attitude of ...

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ژورنال

عنوان ژورنال: European Journal of Control

سال: 2006

ISSN: 0947-3580

DOI: 10.3166/ejc.12.57-70