Method and device for planning modular reconfigurable satellite self-reconfiguration based on hierarchical task network

Abstract

The embodiment of the invention discloses a method for planning modular reconfigurable satellite self-reconfiguration based on a hierarchical task network. The method is applied to a modular reconfigurable satellite and comprises the following steps of: acquiring an initial position matrix corresponding to the initial configuration of a modular reconfigurable satellite and a target position matrix corresponding to a target configuration expected by the self-configuration task of the modular reconfigurable satellite based on a set description coordinate system; determining the moving task of each module in the modular reconfigurable satellite according to the initial position matrix and the target position matrix by using an analytic hierarchy process; and generating a module motion instruction corresponding to each module according to the moving task of each module, wherein the module motion instruction is used for controlling the motion sequence of the motion device installed at each module to perform self-reconfiguration for each module according to the target configuration.

Description

technical field [0001] The embodiment of the present invention relates to the field of satellite technology, in particular to a method, device and computer storage medium for self-reconfiguration of a modular reconfigurable satellite based on hierarchical task network planning. Background technique [0002] Modular reconfigurable satellite is a new concept satellite proposed in order to comply with the development trend of future satellites. It is composed of isomorphic modules with different functions, the same shape and interchangeability. These isomorphic modules can include functional modules such as propulsion modules, navigation modules, and power modules, as well as structural modules and specific payload modules. The overall configuration of the satellite can be changed by moving each isomorphic module, thereby adapting to on-orbit assembly and self-adaptive on-orbit assembly. Orbit services, space pre-deployment to deal with emergencies and other different mission r...

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Problems solved by technology

[0004] In view of the existing conventional technologies mentioned above, when realizing the on-orbit self-reconfiguration task of the modular reconfigurable satellite, the following problems will be brought about: First, the structure span of the linear configuration is relatively large, and the complex space environment where the satellite is located , The damping is small, and the large vibration generated by the linear configuration during the module rotation process is not easy to attenuate; Low energy requirements in missions

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