机译:GFSINS中基于自适应简化球面单纯形无味卡尔曼滤波器的角速度估计
Key Laboratory of Dynamic and Control of Flight Vehicle, Ministry of Education, Beijing Institute of Technology, Beijing, China;
Key Laboratory of Dynamic and Control of Flight Vehicle, Ministry of Education, Beijing Institute of Technology, No. 5, Zhongguancun South Street, Haidian District, Beijing, China;
Key Laboratory of Dynamic and Control of Flight Vehicle, Ministry of Education, Beijing Institute of Technology, Beijing, China;
Key Laboratory of Dynamic and Control of Flight Vehicle, Ministry of Education, Beijing Institute of Technology, Beijing, China;
Gyro-free; angular velocity calculation; Sage-Husa; spherical simplex sampling; unscented Kalman filter;
机译:基于球面单纯形变换修正无味卡尔曼滤波的姿态估计
机译:基于球面单纯形变换修正无味卡尔曼滤波的姿态估计
机译:基于球形单纯形无味卡尔曼滤波器的跳跃和静态相互作用多模型
机译:自适应无味卡尔曼滤波器在GFSINS角速度计算中的应用
机译:无味卡尔曼滤波,用于相对姿态和位置估计。
机译:使用自适应无味卡尔曼滤波器的基于四元数的鲁棒姿态估计
机译:基于改进自适应无需卡尔曼滤波器的锂离子电池的充电状态
机译:Unscented卡尔曼滤波与Unscented schmidt卡尔曼滤波在预测地球同步卫星姿态和相关不确定性中的比较。