Celestial body capturing method based on dynamic small view field

A small field of view, celestial body technology, applied in astronomical navigation, use feedback control, photogrammetry/video measurement, etc., can solve the problems of not being able to adapt to the use requirements of dynamic environments, working mechanism failure, etc., and achieve effective observation of vectors and positions Feedback input, addressing effects of rapid updates

Active Publication Date: 2022-03-01
BEIJING AEROSPACE INST FOR METROLOGY & MEASUREMENT TECH
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Problems solved by technology

[0005] However, in some dynamic applications, such as during the driving process of vehicles or ships, during the initial orbiting, maneuvering and large-angle attitude adjustment of long-range weapons, traditional servo small-field astronomical measurement devices working under static or quasi-static conditions, Limited by its own working principle, it can no longer adapt to the requirements of dynamic environments, and the working mechanism is invalid

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  • Celestial body capturing method based on dynamic small view field
  • Celestial body capturing method based on dynamic small view field
  • Celestial body capturing method based on dynamic small view field

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Embodiment Construction

[0066] In order to enable those skilled in the art to better understand the solutions of the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application.

[0067] The invention aims to provide a method for capturing celestial bodies under dynamic conditions for a small field of view astronomical measurement device. The method decomposes the process of celestial body capturing into two stages: star seeking and tracking. In the star-seeking stage, the fast-updated prior information is used to generate a real-time star-seeking strategy. When the target observation star is selected, the two-axis servo table drives the photoelectric detection unit to rotate to the target celestial body according to the index information and gyroscope information in the star-seeking strategy. Observe the position and make real-time adjustments to...

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Abstract

The invention provides a celestial body capturing method based on a dynamic small view field, and the method comprises the steps: driving a photoelectric detection part to rotate to a target celestial body observation position through the star finding and tracking two-stage operation, carrying out the real-time adjustment, and guaranteeing that the target celestial body is still located in a view field observation range when the shooting moment arrives. Celestial body capture of a small-view-field astronomical measurement device under a dynamic condition is realized, uninterrupted observation vector and position feedback input can be provided for rapid and high-precision position or attitude calculation, and tracking type astronomical measurement based on a single-target celestial body and single-servo active star finding under the dynamic condition is realized; the problems that prior information is rapidly updated and celestial bodies are difficult to capture under the dynamic condition are solved.

Description

technical field [0001] The invention belongs to the field of astronomical measurement, in particular to a method for capturing celestial bodies based on a dynamic small field of view. Background technique [0002] Regarding the celestial body capture method of the dynamic small field of view astronomical measuring device, there is no published patent yet. [0003] The small field of view astronomical measurement device usually works on a two-axis servo platform. According to a certain star-seeking strategy, it searches and captures specific celestial bodies all over the sky. By solving the relationship between the target observation vector and the reference vector, it is obtained The position or attitude information of itself in the local horizon reference system provides stable and accurate calibration input for the inertial navigation system under all-day conditions. [0004] Most of the traditional small-field astronomical measurement devices work in a static or quasi-st...

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Application Information

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IPC IPC(8): G01C11/00G01C21/02G05D3/12
CPCG01C11/00G01C21/025G05D3/12
Inventor商秋芳熊琨裴雅鹏张兴凡王强赵楠楠唐声权刘丽艳吴跃沙春哲刘莎
OwnerBEIJING AEROSPACE INST FOR METROLOGY & MEASUREMENT TECH