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Autonomous safety control method for space optical relative measurement equipment

A relative measurement, space optics technology, applied in TV, color TV parts, electrical components, etc., can solve problems such as camera failure, damage to lens, detection components, endanger product safety, etc., to achieve a clear principle and ensure work. Safe and easy to achieve

Active Publication Date: 2020-11-24
SHANGHAI AEROSPACE CONTROL TECH INST
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AI Technical Summary

Problems solved by technology

When the sun enters the sun protection angle, not only the camera cannot work normally, but also damage the lens, detection components, etc., endangering product safety

Method used

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  • Autonomous safety control method for space optical relative measurement equipment

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Embodiment Construction

[0019] The present invention will be further elaborated below by describing a preferred specific embodiment in detail in conjunction with the accompanying drawings.

[0020] Such as figure 1 As shown, it is a schematic diagram of an autonomous safety control method for a spatial optical relative measurement device according to the present invention. In this embodiment, the spatial optical relative measurement device includes an optical camera.

[0021] Specifically, the autonomous safety control method of the space optical relative measurement equipment includes:

[0022] S1. Determine the relative position of the sun on the orbital plane of the space optical relative measuring equipment, expressed by the inner angle of the sun plane. The inner angle of the solar plane represents the position of the sun on the orbital plane, and at this time, the optical axis of the optical camera in the space optical relative measuring device is at zero position.

[0023] S2. Calculating th...

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Abstract

The invention discloses an autonomous safety control method for space optical relative measurement equipment. The method comprises the steps: S1, determining the relative position of the sun on an operation orbit plane of space optical relative measurement equipment, and representing the relative position through a sun plane interior angle; S2, calculating an included angle between the optical axis of the space optics relative measurement equipment and the solar plane interior angle in the S1, and representing the included angle as a solar incident angle; and S3, executing a corresponding modestate according to a size relationship between the solar incident angle and the solar protection angle threshold of the space optics relative measurement equipment. The method has the advantages thatthe relation among the solar surface interior angle, the solar incident angle and the solar protection angle threshold value is reasonably utilized, the on-orbit operation safety work requirement ofthe space relative measurement equipment is met, the method is clear in principle, convenient to implement and suitable for on-orbit work, and the work safety of the space relative measurement equipment can be guaranteed.

Description

technical field [0001] The invention relates to the field of safe operation of space orbits, in particular to an autonomous safety control method for space optical relative measuring equipment, so as to ensure product safety during orbital operation. Background technique [0002] New requirements such as binary star formation, satellite constellation, and space security have promoted the development of inter-satellite relative measurement technology. A variety of inter-satellite relative measurement products, such as microwave radar, photoelectric combination, and laser radar, are emerging and have been successfully used in orbit. [0003] Usually space optical relative measurement equipment includes photoelectric combination, binocular camera and other products with optical camera as the main body. Due to its detection system, the most important influence of the camera during its work in space is the sun. Space cameras have an important indicator: the sun protection angle...

Claims

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Application Information

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IPC IPC(8): H04N5/232
CPCH04N23/667H04N23/695
Inventor 张朝兴邵志杰孙尚戴维宗王静吉袁彦红张小伟
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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