Self-reconstitution cell star device

Abstract

The invention relates to the technical field of cell robot manufacturing, in particular to a method for sensing the posture of a user through a control assembly and a visual capture mechanism, conducting task analysis through a control computer so as to generate a space topological structure and an optimal interface splicing decision needed by tasks, conducting mutual splicing through a six-direction thrust device, and conducting multi-dimensional splicing through the six-direction thrust device. The self-reconfiguration cell star device comprises a box body (1), an angle-adjustable side plate (2), a rotary top plate (3), a control assembly, a universal docking port (5), a six-direction thrust device (6), a heat sensor (7), a visual capturing mechanism (8), an electrical interface (9), a driving assembly (10), a storage battery (11), a propellant module (12) and a control computer (13). The cell star has the advantages of being self-adaptive, high in expansibility, decentralized, open in architecture, economical and the like, can fully adapt to the complexity of future space tasks, and has reference significance for on-orbit spacecraft configuration.

Description

technical field [0001] The present invention relates to the technical field of cell robot manufacturing, specifically a method of sensing its own posture through control components and a visual capture mechanism, and using a control computer to perform task analysis to generate the space topology required for the task and the optimal interface splicing decision. Relying on the six-way thrust device for mutual splicing, and then completing the self-reconfiguration construction of the spacecraft required for the mission, and relying on internal motion to realize the self-reconfiguration cell-star device of the spacecraft's shape change. Background technique [0002] With the rapid development of space science and technology, the characteristics of its missions tend to be diverse, complex and unknown. Compared with traditional spacecraft, the current modular spacecraft has greatly shortened the time period in the design, manufacturing and deployment stages, but there are still ...

AI Technical Summary

Problems solved by technology

Compared with traditional spacecraft, the current modular spacecraft has greatly shortened the time period in the design, manufacturing and deployment stages, but there are still problems such as high cost, simple function, poor versatility, and poor reconfiguration and upgrade capabilities

Constrained by the size of the launch vehicle fairing, the maximum size of the spacecraft manufactured on the ground is also strictly limited

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