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Clustering-grade satellite fault tolerance control method based on nonlinear planning

A non-linear planning, fault-tolerant control technology, applied in the field of aerospace satellite formation control

Active Publication Date: 2018-10-02
TIANJIN UNIV
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Problems solved by technology

Aiming at the problem of satellite faults in deep space exploration tasks based on satellite formations, the present invention proposes a new satellite formation fault-tolerant strategy, studies the trajectory planning of faulty satellites leaving formations and backup satellites entering formations during formation reconfiguration maneuvers, and realizes fault-free The reconstruction of the entire satellite formation configuration is universal for satellite formations of any configuration. It is a useful exploration for the use of micro-satellite formations to realize deep space exploration technology, and at the same time provides a solution for high-precision flight of micro-satellite formations under satellite failures. new ideas

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  • Clustering-grade satellite fault tolerance control method based on nonlinear planning
  • Clustering-grade satellite fault tolerance control method based on nonlinear planning
  • Clustering-grade satellite fault tolerance control method based on nonlinear planning

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Embodiment Construction

[0124] The present invention aims at completing the deep space exploration mission in the sub-satellite point horizontal circle formation configuration, assuming that one of the slave satellite actuators, sensors or on-board radars in the satellite formation fails, making it difficult for the entire formation to reach The required mission accuracy requirements, in this case, the present invention proposes a satellite formation fault-tolerant control strategy 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, and determining the fault satellite The best position to leave the formation, so that the faulty star exits the formation, and timely replenishes the new backup star to enter the formation, finds the best position for the backup star to enter the formation and the best start time for maneuvering, so as to ensure that the faulty star can be fully rep...

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Abstract

The invention relates to a clustering-grade satellite fault tolerance control method. A proper and effective satellite formation fault tolerance control strategy is designed for a deep space detectionsystem based on the minimal satellite formation technology, so the formation satellite is capable of adjusting the formation types by use of the nonlinear dynamic planning technology in case of a failure so as to continue to finish task requirements. According to the invention, based on the clustering-grade satellite fault tolerance control method, after the satellite fails in a formation process, by determining initial and termination positions of the fault satellite and a standby satellite, considering inter-satellite collision and time constraints, and taking the fuel consumption as a performance index, by use of the Gauss pseudo-spectral method, the optimal leaving and entering positions of the fault satellite and the standby satellite are determined and respective optimal track plansare acquired, so it is ensured that the position of the fault satellite can be completely filled through the entering the standby satellite, and the standby satellite and the healthy satellites forma new formation, thereby achieving performance requirements of the formation. The method is mainly applied in clustering-grade satellite fault tolerance control occasions.

Description

technical field [0001] The invention relates to a fault-tolerant fault-tolerant control method for constellation-level satellites based on nonlinear programming, which is mainly used in the process of formation reconstruction when formation satellites fail when they are in orbit, and belongs to the field of aerospace satellite formation control. Specifically, it involves a fault-tolerant control method for constellation-level satellites based on nonlinear programming. Background technique [0002] In recent years, with the continuous complexity of space mission requirements, the traditional single satellite is far from meeting the mission requirements. The vigorous development of micro-satellite technology has made multiple satellites form formations to work together to complete complex mission objectives, which has become the mainstream direction of space technology development. Multi-satellite formation flight means that multiple satellites maintain a space configuration ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 田栢苓张秀云宗群
Owner TIANJIN UNIV
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