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Angular velocity estimation from measurement vectors of star tracker

机译:根据恒星跟踪仪的测量矢量估算角速度

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摘要

In most spacecraft, there is a need to know the craft's angular rate. Approaches with least squares and an adaptive Kalman filter are proposed for estimating the angular rate directly from the star tracker measurements. In these approaches, only knowledge of the vector measurements and sampling interval is required. The designed adaptive Kalman filter can filter out noise without information of the dynamic model and inertia dyadic. To verify the proposed estimation approaches, simulations based on the orbit data of the challenging minisatellite payload (CHAMP) satellite and experimental tests with night-sky observation are performed. Both the simulations and experimental testing results have demonstrated that the proposed approach performs well in terms of accuracy, robustness, and performance.
机译:在大多数航天器中,需要知道航天器的角速度。提出了具有最小二乘法和自适应卡尔曼滤波器的方法,用于直接从恒星跟踪器测量结果估算角速率。在这些方法中,仅需要了解矢量测量和采样间隔。设计的自适应卡尔曼滤波器可以滤除噪声,而无需动力学模型和惯性二阶信息。为了验证提出的估算方法,基于具有挑战性的微型卫星有效载荷(CHAMP)卫星的轨道数据进行了仿真,并进行了具有夜空观测的实验测试。仿真和实验测试结果均表明,该方法在准确性,鲁棒性和性能方面表现良好。

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