Attitude control laws validation through probabilistic µ-analysis: application to microsatellite control laws
Résumé
With the growing complexity of space missions, the validation & verification (V&V) phase in AOCS design becomes very time-consuming. Based on a realistic microsatellite design example, the objective of this paper is to show how recent advances in the development of μ-analysis and probabilistic μ-analysis tools can be used to improve the efficiency of controllers' robustness analysis before the Monte-Carlo simulation campaigns. More precisely, after a brief presentation of the tools, it is shown how they can be integrated in a current V&V process and what can be expected next.
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