Ground calibration device and calibration method for in-orbit mass measurement instrument

A quality measurement and calibration device technology, applied in the aerospace field, can solve problems such as failure to meet calibration requirements, short duration, high cost, etc., and achieve the effect of fast and efficient calibration

Pending Publication Date: 2018-03-06
四川航天计量测试研究所
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Problems solved by technology

The on-orbit mass measuring instrument is a mass measuring device used in a microgravity environment. In order to complete the measurement and calibration of the device, it is necessary to simulate the weightlessness state in the ground environment. However, the weightlessness environment generated by the drop tower and the parabolic flight of the aircraft are usually used. , short duration, unable to meet calibration requirements, and expensive

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  • Ground calibration device and calibration method for in-orbit mass measurement instrument

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Embodiment Construction

[0026] Below in conjunction with accompanying drawing, the present invention is described in detail.

[0027] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0028] Such as figure 1 As shown, a ground calibration device for an on-orbit mass measuring instrument includes a microgravity environment simulation device and a calibration process state monitoring system, and the microgravity environment simulation device includes a high tower suspension mechanism 1 and an adjustable horizontal workbench 2. The calibration process state monitoring system includes a suspension rope tension monitoring module 3, a measured object deflection angle monitoring modu...

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Abstract

The invention discloses a ground calibration device for an in-orbit mass measurement instrument. The ground calibration device comprises a microgravity environment simulation device and a calibrationprocess state monitoring system. The microgravity environment simulation device comprises a high tower suspension mechanism and an adjustable horizontal workbench. The calibration process state monitoring system comprises a suspension rope tension monitoring module, a tested object deflection angle monitoring module and a tested object acceleration monitoring module. By aerial suspension for gravity counteraction, a microgravity environment is simulated on a water plane close to a suspension balance point; by the established calibration process state monitoring system for real-time monitoringof a calibration process, whether the calibration process meets set boundary conditions or not can be judged, and an in-orbit mass measurement instrument indicating value corresponding to the measurement process meeting the set boundary conditions is determined as a ground calibration effective value, so that a brand-new solution approach is provided for ground calibration of the in-orbit mass measurement instrument. The ground calibration device has advantages that effective calibration of the in-orbit mass measurement instrument in a ground environment is realized while calibration operationis standardized, and metrological guarantee is provided for equipment used in the special environment.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and in particular relates to a calibration device and a calibration method for a mass measuring instrument used in an orbital microgravity environment in a ground environment. Background technique [0002] The equipment for mass measurement using Newton's second law in the on-orbit microgravity environment is hereinafter referred to as the on-orbit mass measuring instrument. The on-orbit mass measuring instrument is a mass measuring device used in a microgravity environment. In order to complete the measurement and calibration of the device, it is necessary to simulate the weightlessness state in the ground environment. However, the weightlessness environment generated by the drop tower and the parabolic flight of the aircraft are usually used. , the duration is short, the calibration requirements cannot be met, and the cost is expensive. Contents of the invention [0003] The object of the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01G23/01
CPCG01G23/015
Inventor 马仕才朱玥高育帼徐萍胡喜祥
Owner 四川航天计量测试研究所
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