机译:基于火星进入时无偏最小方差估计的自主导航方法
Research Center of Small Sample Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
Research Center of Small Sample Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
Research Center of Small Sample Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
Army Aviation Research Institute, Beijing 101123, China;
Research Center of Small Sample Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
Autonomous navigation; Measurement systematic errors; Unknown inputs; Extension of unbiased minimum-variance; Mars entry;
机译:非线性非偏见最小方差滤波器,用于大不确定性和未知测量偏差下的火星入口自主导航
机译:具有未知输入的非线性系统基于Unscented卡尔曼滤波器的无偏最小方差估计
机译:基于最小方差无偏估计的时变风荷载识别
机译:基于假设的“快看”进入导航数据评估火星进入重建轨迹
机译:信息有限的城市自动驾驶估算与导航方法
机译:基于模型的惯性矩估计的自主导航
机译:基于序列图像的自主导航和危害避免方法MARS软着陆
机译:基于假设“快速查看”进入导航数据的火星进入重建轨迹评估