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深空探测中光学导航相机在轨标定方法

On-orbit calibration approach for optical navigation camera in deep space exploration.

作者信息

Wang Mi, Cheng Yufeng, Yang Bo, Jin Shuying, Su Hongbo

出版信息

Opt Express. 2016 Mar 7;24(5):5536-5554. doi: 10.1364/OE.24.005536.

Abstract

A spacecraft-borne optical navigation camera is one of the key instruments for optical autonomous navigation, and the line of sight (LOS) of the camera directly affects the accuracy of navigation. We developed an on-orbit calibration approach for a navigation camera to ensure the accuracy, in which a stepwise calibration is performed, external parameters estimated, and internal parameters estimated in a generalized camera frame determined by external parameters. In addition, we proposed a batch and sequential on-orbit estimation method to save on-orbit computing power, and established a strategy to reject misidentified reference stars while keeping consistency in on-orbit parameters estimation. After the calibration, the accuracy of LOS in inertial frame satisfied the need in optical autonomous navigation. The results have been proven precise and robust in three experiments.

摘要

航天器搭载的光学导航相机是光学自主导航的关键仪器之一,相机的视线(LOS)直接影响导航精度。我们开发了一种用于导航相机的在轨校准方法以确保精度,该方法进行逐步校准、估计外部参数,并在由外部参数确定的广义相机坐标系中估计内部参数。此外,我们提出了一种批处理和顺序在轨估计方法以节省在轨计算能力,并建立了一种在保持在轨参数估计一致性的同时拒绝误识别参考星的策略。校准后,惯性系中视线的精度满足了光学自主导航的需求。结果在三个实验中已被证明是精确且稳健的。

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