On-orbit calibration for star sensors without priori information

被引:30
|
作者
Zhang, Hao [1 ]
Niu, Yanxiong [1 ]
Lu, Jiazhen [1 ]
Zhang, Chengfen [1 ]
Yang, Yanqiang [1 ]
机构
[1] Beihang Univ, Sch Instrumentat Sci & Optoelect Engn, Beijing 100191, Peoples R China
来源
OPTICS EXPRESS | 2017年 / 25卷 / 15期
关键词
BATCH ESTIMATION; NEURAL-NETWORKS; TRACKER; PERFORMANCE; ALIGNMENTS; SYSTEMS;
D O I
10.1364/OE.25.018393
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
The star sensor is a prerequisite navigation device for a spacecraft. The on-orbit calibration is an essential guarantee for its operation performance. However, traditional calibration methods rely on ground information and are invalid without priori information. The uncertain on-orbit parameters will eventually influence the performance of guidance navigation and control system. In this paper, a novel calibration method without priori information for on-orbit star sensors is proposed. Firstly, the simplified back propagation neural network is designed for focal length and main point estimation along with system property evaluation, called coarse calibration. Then the unscented Kalman filter is adopted for the precise calibration of all parameters, including focal length, main point and distortion. The proposed method benefits from self-initialization and no attitude or preinstalled sensor parameter is required. Precise star sensor parameter estimation can be achieved without priori information, which is a significant improvement for on-orbit devices. Simulations and experiments results demonstrate that the calibration is easy for operation with high accuracy and robustness. The proposed method can satisfy the stringent requirement for most star sensors. (C) 2017 Optical Society of America
引用
收藏
页码:18393 / 18409
页数:17
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