Satellite geometric feature and attitude estimation method based on foundation observation luminosity signal

A technology of attitude estimation and geometric features, applied in the field of space optical information processing, can solve problems such as difficulty in obtaining accurate geometric features, difficulty in carrying out attitude estimation work, and inability to directly apply space target attitude parameter estimation, so as to improve simulation accuracy and realize The effect of low difficulty and low cost

Active Publication Date: 2021-08-03
HARBIN INST OF TECH
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However, most current studies on photometric curves still have some limitations. On the one hand, these studies are mostly based on the known geometric model of the target, but in fact, the accurate geometric characteristics of the target are difficult to obtain, leading t

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  • Satellite geometric feature and attitude estimation method based on foundation observation luminosity signal
  • Satellite geometric feature and attitude estimation method based on foundation observation luminosity signal
  • Satellite geometric feature and attitude estimation method based on foundation observation luminosity signal

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[0097] 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 making creative efforts belong to the protection scope of the present invention.

[0098] The object of the present invention is to provide a satellite geometric feature and attitude estimation method based on the ground-based observation photometric signal, using the satellite time-series photometric signal of the ground-based observation as input, and using the satellite geometric database and the satellite attitude kinematic equation to identify the geometric features of the satellite , on this basis, update the state of the space target a...

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Abstract

The invention discloses a satellite geometric feature and attitude estimation method based on a foundation observation luminosity signal. The method comprises the following steps: S1, establishing a satellite luminosity signal observation model under a foundation observation condition; S2, establishing a 'geometry-attitude-luminosity' database of the satellite; S3, identifying a geometric model and a scale of the satellite; S4, establishing an attitude kinematics equation of the observed satellite; S5, setting an initial parameter of the non-destructive Kalman filter; S6, taking the attitude kinematics equation and the satellite luminosity signal observation model as a time updating model and an observation updating model of a non-destructive Kalman filtering algorithm respectively, and performing updating estimation on satellite attitude parameters at the next observation moment by adopting the non-destructive Kalman filtering algorithm; and S7, taking the satellite attitude parameter estimated in the step S6 as a new observation moment satellite state parameter, repeating the step S6, and stopping iteration when the error of a satellite attitude parameter estimation value is smaller than a set threshold value or the satellite exceeds an observation range so as to obtain a high-precision satellite attitude parameter estimation value.

Description

technical field [0001] The invention relates to the technical field of space optical information processing, in particular to a satellite geometric feature and attitude estimation method based on ground-based observation photometric signals. Background technique [0002] In recent years, the increasingly tense space resources and international relations have put forward higher and newer requirements for the space situational awareness capabilities of countries. Accurate identification of key features of space targets is one of the main tasks of space situational awareness, and is of great significance to tasks such as target type identification, status judgment, threat assessment, and strategic decision-making. The ground-based photometric signal only contains energy information, which is the result of the coupling of various key features of the space target. It can comprehensively reflect the time series changes of the geometric shape, scale and attitude of the space target...

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Application Information

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IPC IPC(8): G06F30/23
CPCG06F30/23
Inventor 智喜洋鲍广震巩晋南张寅胡建明施天俊张鹏飞
Owner HARBIN INST OF TECH
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