High Update Rate Star Tracker for Gyroless Spacecraft Operation

Mikael Marin, H. Bang
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引用次数: 1

Abstract

Traditional star trackers are designed for high accuracy but low update rate and rely on rate gyros to interpolate between measurements. However, the available rate gyros are either noisy, or expensive and heavy. The proposed work demonstrates the advantage of sacrificing some of the star tracker's accuracy for a higher update rate. As a result, aside from removing the need for a rate gyro, Attitude Determination and Control Systems overall performances are increased. The proposed star tracker achieved a 0.001 ° accurate Attitude Determination, with a 98.8% sky coverage at a 50Hz update rate. In addition, the image processing and star matching algorithm are designed to be efficiently implemented as a fully pipelined single-pass FPGA circuit.
用于无陀螺航天器运行的高更新率星跟踪器
传统的星跟踪器精度高,但更新率低,并且依靠速率陀螺仪在测量之间进行插值。然而,现有的速率陀螺仪要么噪声大,要么价格昂贵且笨重。所提出的工作证明了牺牲一些星跟踪器的精度以获得更高的更新率的优势。因此,除了消除对速率陀螺仪的需求外,姿态确定和控制系统的整体性能也得到了提高。提出的星跟踪器实现了0.001°的精确姿态确定,在50Hz更新速率下具有98.8%的天空覆盖率。此外,图像处理和星型匹配算法被设计成一个全流水线的单通FPGA电路。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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