The geomagnetic localization based on the ICCP algorithm can be used to bind the position errors inherent in Inertial Navigation System(INS), which increases with time.
基于ICCP算法的地磁匹配定位可以用于限制惯导系统随时间增长的位置误差。
2
Variations on which attitude of spacecraft dependents are time, law of motion of manipulators, liquid mass, liquid inertial tensor and damping coefficient besides paths of motion of manipulators.