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Ground variable center of mass zero gravity simulation device and simulation method

A technology of a simulation device and a simulation method, which is applied in the simulation device of space navigation conditions, transportation and packaging, space navigation equipment, etc., and can solve the problems affecting the performance of space equipment.

Active Publication Date: 2022-04-29
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Aiming at the problem that existing microgravity simulation devices affect the performance of space devices, the present invention provides a zero-gravity simulation device and simulation method with ground variable center of mass

Method used

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  • Ground variable center of mass zero gravity simulation device and simulation method
  • Ground variable center of mass zero gravity simulation device and simulation method
  • Ground variable center of mass zero gravity simulation device and simulation method

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Embodiment Construction

[0086] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0087] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0088] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments, but not as a limitation of the present invention.

[0089] The ground variable center of mass zero-gravity simulation device of this embodiment includes a base 1, a...

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Abstract

The ground variable center of mass zero-gravity simulation device and simulation method solve the problem that the existing micro-gravity simulation device affects the performance of space devices, and belong to the field of ground zero-gravity simulation in space. The spherical air bearing seat is placed on the base of the present invention; the spherical air bearing seat supports the spherical air bearing rotor, and a layer of air film is formed between the middle platform and the spherical air bearing rotor, so that the middle platform is air-floated; the middle platform , the lower platform, the Z-direction movement module, the linear module fixed platform, the XY-direction movement module, and the upper platform are connected from bottom to top in sequence; The detected change of the center of mass controls the XY direction movement module, the Z direction movement module and the air injection of the spherical air bearing rotor, so that the center of mass of the integrated part moves to the center of the spherical air bearing rotor to realize the adjustment of the center of mass.

Description

technical field [0001] The invention relates to the field of ground zero-gravity simulation in space, in particular to a ground-variable center-of-mass zero-gravity simulation device and a simulation method applied to a space-variable center-of-mass device. Background technique [0002] With the continuous development of aerospace technology, the tasks that humans can achieve in space are more diverse, and the operating equipment is also becoming larger, more complex, and more scalable. When controlling a large and variable space device such as a space station connected to a space manipulator, it is necessary to consider that when the manipulator moves, the center of mass of the entire space device will change, and the change of the center of mass means the coordinate transformation between each sub-body The relationship has changed. At this time, if the previous coordinate transformation relationship is used, the control will deviate, which may lead to the failure of the sp...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G7/00
CPCB64G7/00
Inventor 姚蔚然张欧阳杜德嵩刘健行孙光辉吴立刚
Owner HARBIN INST OF TECH
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