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Ground virtual verification system and method for spacecraft on-orbit maintenance

A verification system and spacecraft technology, applied in the direction of instrumentation, mechanical mode conversion, calculation, etc., can solve the problems of high cost, complex system, long test cost and cycle of neutral buoyancy simulator, and achieve low cost and test cost, The effect of wide application range and real-time evaluation of maintenance effect

Active Publication Date: 2019-03-26
BEIJING SPACE TECH RES & TEST CENT
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AI Technical Summary

Problems solved by technology

The neutral buoyancy simulator can be used to complete the ground verification of on-orbit maintenance of manned spacecraft, but the neutral buoyancy simulator used in this verification method is expensive, the system is complex, and the cost and cycle of each test are long

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  • Ground virtual verification system and method for spacecraft on-orbit maintenance

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Embodiment Construction

[0030] The description of the embodiments of this specification should be taken in conjunction with the corresponding accompanying drawings, which should be made a part of the complete specification. In the drawings, the shapes or thicknesses of the embodiments may be enlarged and indicated for simplicity or convenience. Furthermore, the parts of each structure in the drawings will be described with separate descriptions. It is worth noting that the elements not shown in the drawings or described by text are in the form known to those of ordinary skill in the art.

[0031] The description of the embodiments herein, and any reference to the direction and orientation, are only for the convenience of description, and should not be construed as any limitation on the protection scope of the present invention. The following description of the preferred embodiments will involve combinations of features, and these features may exist independently or in combination, and the present inv...

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Abstract

The invention relates to a spacecraft on-orbit maintenance ground virtual verification system. The spacecraft on-orbit maintenance ground virtual verification system comprises a human-machine interaction system, a virtual scene system, an external display system and a maintenance evaluation system, and the human-machine interaction system is used for displaying the virtual on-orbit maintenance process for a spaceman in trial and completing virtual on-orbit operations through data gloves with force feedback; the virtual scene system is used for simulating the on-orbit maintenance scene and process of a spacecraft; the external displaying system is used for displaying the virtual on-orbit maintenance process and maintenance data; the maintenance evaluation system is used for evaluating the on-orbit maintenance effect according to the virtual on-orbit maintenance process and the maintenance data displayed by the external displaying system and modifying the maintenance scheme according tothe evaluation result. The invention further relates to a spacecraft on-orbit maintenance ground virtual verification method implemented through the system.

Description

technical field [0001] The invention relates to a virtual verification system and method for the on-orbit maintenance of a spacecraft on the ground. Background technique [0002] Objects in space are in a weightless state, and astronauts’ actions in space are difficult to control. Many maintenance methods that are considered reasonable on the ground may not work in space. To ensure the success of on-orbit maintenance, ground verification and training trials of on-orbit maintenance must be carried out on the ground. [0003] At present, the widely used on-orbit maintenance ground verification method is to conduct neutral buoyancy simulation test on the ground. For example, ground-based simulations of Hubble's in-orbit repairs are carried out in the neutral buoyancy simulator at the Marshall Space Flight Center. A full-scale model of the Hubble telescope, equipment to be replaced and maintenance tools are placed in the simulator, and the astronauts wear diving pressure suits...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F3/01G06Q10/00
CPCG06F3/012G06F3/014G06F3/016G06F2203/012G06F2203/014G06Q10/20
Inventor 张伟杨宏李兴乾刘铭王岩李涛李志海李伟夏侨丽王为张健
Owner BEIJING SPACE TECH RES & TEST CENT
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