A fault-tolerant control method for constellation-level satellites based on nonlinear programming
A nonlinear programming and fault-tolerant control technology, applied in the field of aerospace satellite formation control
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[0124] The present invention is aimed at the process of the satellite completing the deep space exploration mission in the horizontal circle formation configuration of the sub-satellite point. It is assumed that one of the satellite actuators, sensors or on-board radar in the satellite formation fails, making it difficult for the entire formation to reach the target. The required mission accuracy is required. In this case, the present invention proposes a fault-tolerant control strategy for satellite formation based on nonlinear programming for the first time; by taking the overall performance of the satellite formation as the realization goal, considering the fuel consumption problem, the faulty satellite is determined. The best position to leave the formation is to make the faulty star exit the formation, and a new backup star will be added to the formation in a timely manner, and the best position of the backup star to enter the formation and the best start time of maneuverin...
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