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A multi-objective six-degree-of-freedom microgravity ground simulation system and using method

A technology of ground simulation and degree of freedom, applied to the simulation device of space navigation conditions, space navigation equipment, transportation and packaging, etc., to achieve the effect of strong stability, simple structure and large number of simulations

Active Publication Date: 2022-07-15
HARBIN INST OF TECH
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Problems solved by technology

[0005] The purpose of the present invention is to propose a multi-objective six-degree-of-freedom microgravity ground simulation system and its application method to solve the problems existing in the prior art

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  • A multi-objective six-degree-of-freedom microgravity ground simulation system and using method
  • A multi-objective six-degree-of-freedom microgravity ground simulation system and using method
  • A multi-objective six-degree-of-freedom microgravity ground simulation system and using method

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Embodiment Construction

[0039] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0040] refer to figure 1As shown, the present invention proposes a multi-objective six-degree-of-freedom microgravity ground simulation system. The multi-objective six-degree-of-freedom microgravity ground simulation system includes a high-rigidity gantry 1, a discrete guiding system 2, a six-degree-of-freedom simulation platform 3, Motion Measurement System 4,

[0041] The high-rigidity gantry 1 is fixed on the ground, the discrete ...

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Abstract

The invention discloses a multi-target six-degree-of-freedom microgravity ground simulation system and a using method, which belong to the technical field of ground microgravity simulation test. Including high-rigidity gantry, discrete guiding system, 6-DOF simulation platform, motion measurement system, high-rigidity gantry is fixed on the ground, discrete guiding system is installed on the lower surface of high-rigidity gantry, 6-DOF simulation platform It is slidably connected with the discrete guide system and suspended below the discrete guide system, and the motion measurement system is installed around the high-rigidity gantry. The present invention allows no less than five six-degree-of-freedom simulation platforms to perform ground simulation motion at the same time, adopts a combined two-dimensional motion system and a vertical lifting system to track the spatial position, the three-degree-of-freedom rotation system adapts to the spatial attitude, and the constant force maintaining system provides micro The gravity environment enables the whole system to adapt to the six-degree-of-freedom load and the large-scale maneuvering and multi-load staggered motion simulation.

Description

technical field [0001] The invention relates to a multi-target six-degree-of-freedom microgravity ground simulation system and a using method, and belongs to the technical field of ground microgravity simulation test. Background technique [0002] With the continuous development of space science and technology, whether it is near-Earth navigation or deep space exploration, the frequency of spacecraft research and development is getting higher and higher, the system functions are becoming more and more complex, and the frequency of verifying new technologies and solutions is increasing. However, spacecraft have high technical risks, complex system functions, high launch costs, and large losses due to test failures. In order to minimize the losses caused by spacecraft failures or failures, it is particularly important to ensure high spacecraft reliability. Therefore, it is the basic guarantee for the success of the launch mission to conduct as many test simulations based on th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G7/00
CPCB64G7/00
Inventor 刘延芳周芮齐乃明佘佳宇齐骥倪晨瑞王旭霍明英赵钧刘振
Owner HARBIN INST OF TECH