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一种新型光学系统误差模型及星敏感器在轨标定方法。

A Novel Error Model of Optical Systems and an On-Orbit Calibration Method for Star Sensors.

作者信息

Wang Shuang, Geng Yunhai, Jin Rongyu

机构信息

Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China.

出版信息

Sensors (Basel). 2015 Dec 12;15(12):31428-41. doi: 10.3390/s151229863.

Abstract

In order to improve the on-orbit measurement accuracy of star sensors, the effects of image-plane rotary error, image-plane tilt error and distortions of optical systems resulting from the on-orbit thermal environment were studied in this paper. Since these issues will affect the precision of star image point positions, in this paper, a novel measurement error model based on the traditional error model is explored. Due to the orthonormal characteristics of image-plane rotary-tilt errors and the strong nonlinearity among these error parameters, it is difficult to calibrate all the parameters simultaneously. To solve this difficulty, for the new error model, a modified two-step calibration method based on the Extended Kalman Filter (EKF) and Least Square Methods (LSM) is presented. The former one is used to calibrate the main point drift, focal length error and distortions of optical systems while the latter estimates the image-plane rotary-tilt errors. With this calibration method, the precision of star image point position influenced by the above errors is greatly improved from 15.42% to 1.389%. Finally, the simulation results demonstrate that the presented measurement error model for star sensors has higher precision. Moreover, the proposed two-step method can effectively calibrate model error parameters, and the calibration precision of on-orbit star sensors is also improved obviously.

摘要

为了提高星敏感器在轨测量精度,本文研究了在轨热环境引起的像面旋转误差、像面倾斜误差以及光学系统畸变等因素。由于这些问题会影响星像点位置的精度,本文在传统误差模型的基础上探索了一种新型测量误差模型。由于像面旋转倾斜误差具有正交特性且这些误差参数之间存在强非线性,难以同时对所有参数进行标定。为解决这一难题,针对新的误差模型,提出了一种基于扩展卡尔曼滤波器(EKF)和最小二乘法(LSM)的改进两步标定方法。前者用于标定主点漂移、焦距误差以及光学系统畸变,后者用于估计像面旋转倾斜误差。采用这种标定方法,受上述误差影响的星像点位置精度从15.42%大幅提高到1.389%。最后,仿真结果表明所提出的星敏感器测量误差模型具有更高的精度。此外,所提出的两步法能够有效标定模型误差参数,在轨星敏感器的标定精度也得到了明显提高。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/7d64/4721783/25b6276445fe/sensors-15-29863-g001.jpg

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