机译:使用矢量观测值的迭代乘法扩展卡尔曼滤波器用于姿态估计
Department of Navigation Engineering Naval University of Engineering Jiefang Rd. 717, Qiaokou District, Wuhan, 430033 China;
Department of Navigation Engineering Naval University of Engineering Jiefang Rd. 717, Qiaokou District, Wuhan, 430033 China;
Department of Navigation Engineering Naval University of Engineering Jiefang Rd. 717, Qiaokou District, Wuhan, 430033 China;
Quaternions; Estimation; Space vehicles; Q measurement; Kalman filters; Kinematics; Mathematical model;
机译:使用协方差膨胀乘扩展卡尔曼滤波器从不确定传感器观测到的鲁棒姿态估计
机译:用于使用实际数据进行连续航天器姿态估计的非线性滤波:Cubature Kalman滤波,Unscented Kalman滤波和Extended Kalman滤波
机译:具有真实数据的连续航天器姿态估计的非线性滤波:Cubature Kalman滤波器,Unscented Kalman滤波器和扩展卡尔曼滤波器
机译:基于陀螺和矢量观测的高效扩展卡尔曼滤波用于姿态估计
机译:通过扩展卡尔曼滤波器的四轴飞行器姿态估计。
机译:基于矢量观测的用于姿态估计的顺序乘法扩展卡尔曼滤波器
机译:使用载体观测的姿态估计顺序乘法扩展卡尔曼滤波器