This paper aims to introduce a novel approach for designing the Attitude Determination and Control System (ADCS) of spacecraft. The goal is to ensure reliability and pointing performance under constraints such as low power consumption and mass. The approach is based on a structure/controller co-design using Structured H_∞ Synthesis in Matlab which has the great advantage to be easily applicable to any controlled system. Even if co-designing controlled system used to be a hard task, using Structured H_∞ Synthesis brings a new perspective in this field.
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