Adaptive unscented Kalman filter based on sequential state difference for spacecraft autonomous navigation during the approach phase

作者：Wenjia Zhang, Xin Ma, Shuting Wang, Peiling Cui, Xiaolin Ning · 发表于：Measurement · 年份：2024 · DOI：10.1016/j.measurement.2024.116330 · 被引用次数：12 · 研究领域：Inertial Sensor and Navigation、Target Tracking and Data Fusion in Sensor Networks、GNSS positioning and interference