Remote sensing camera on-orbit geometric calibration method based on fixed star trajectory

A remote sensing camera and geometric calibration technology, which is applied in the field of remote sensing satellite geometric positioning, can solve the problems of high control point extraction accuracy requirements and complex calculations, and achieves the effect of strong universality, high accuracy, and improved on-orbit positioning accuracy.

Pending Publication Date: 2021-03-02
SHANGHAI INST OF TECHNICAL PHYSICS - CHINESE ACAD OF SCI
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Problems solved by technology

When the remote sensing camera performs geometric calibration based on the ground control points, the geometric calibration field or DEM / DOM products are generally used to obtain the ground control points. Influenced by various factors, when the remote sensing camera performs geometric calibration based on star observation, it often needs to observe a large number of stars in the field of view of the camera, so when the camera only observes a small number of stars, the calibration method is limited

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  • Remote sensing camera on-orbit geometric calibration method based on fixed star trajectory
  • Remote sensing camera on-orbit geometric calibration method based on fixed star trajectory
  • Remote sensing camera on-orbit geometric calibration method based on fixed star trajectory

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[0061] The flow of the on-orbit geometric calibration method for remote sensing cameras based on stellar trajectories is as follows: figure 1 As shown below, taking a geostationary orbit multispectral staring camera with a focal plane of 512×512 as an example, the embodiment of the present invention will be further described in detail in conjunction with the accompanying drawings:

[0062] 1. Depending on the pointing angle of the boresight of the camera, the stars imaged in the focal plane of the camera are different. According to the stellar prediction plan, adjust the east-west and north-south pointing angles of the camera through instructions, so that the camera pointing mirror points to different sky areas, and realizes the observation of the target star. Continuously observe the stars through the camera to obtain star maps;

[0063] 2. If figure 2 As shown in Fig. 1, the Gaussian surface fitting method is used to extract the sub-pixel centroid of the star target, and ...

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Abstract

The invention discloses a remote sensing camera on-orbit geometric calibration method based on a fixed star trajectory. The method comprises the following steps: (1) acquiring a star map; (2) acquiring a high-precision fixed star position by adopting a centroid extraction algorithm; (3) performing curve fitting on the fixed star position and removing abnormal points to obtain a fixed star track; (4) establishing a camera strict imaging geometric positioning model based on the collinear equation and the generalized pointing angle model; (5) calculating object space vectors of the fixed star track points at different moments according to the right ascension and declination and ephemeris data of the fixed star; and (6) resolving internal and external calibration parameters based on space resection and a least square method to achieve high-precision geometric calibration. According to the method, when the number of fixed stars in the field of view is small, on-orbit geometric calibration of the remote sensing camera can be achieved by utilizing the track of the fixed stars sliding over the image plane, the problem that geometric positioning precision is affected due to the fact that ground control points are difficult to obtain due to cloud shielding is effectively solved, and the method is small in calculated amount, high in precision and high in robustness.

Description

technical field [0001] The invention mainly relates to the technical field of geometric positioning of remote sensing satellites, in particular to an on-orbit geometric calibration method of a geostationary orbit remote sensing camera. Background technique [0002] Remote sensing cameras are usually calibrated on the ground before launch, including the calibration of the internal distortion of the camera and the calibration of the installation relationship of the camera relative to the attitude control system. However, due to the complex structure of the camera and the large size of the optical parts, the acceleration and shock vibrations endured during the launch process, the changes in the surrounding environment during orbital operation, and the thermal radiation from the sun will make each parameter or model deviate from the calibration value on the ground. It will affect the high-precision target positioning, so the on-orbit calibration of the spaceborne camera is requi...

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Application Information

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IPC IPC(8): G06T7/80G06T7/66
CPCG06T7/80G06T7/66G06T2207/10032
Inventor 陈凡胜李潇雁江林逸杨林
Owner SHANGHAI INST OF TECHNICAL PHYSICS - CHINESE ACAD OF SCI
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