inertial mode meaning in Chinese

惯性工作状态
惯性模

In order to improve the convergence properties , unscented kalman filter ( ukf ) algorithm is derived under stellar - inertial modes
为了改善收敛性能,提出了在星敏感器与光纤陀螺联合定姿模式下的unscented卡尔曼滤波算法。
This paper presents and probes into several filtering schemes for the deep space explores attitude measurement system composed of star sensors and gyros . under the stellar - inertial modes , two attitude determination algorithms are designed which use the extended kalman filter . one of the algorithms is to linearized the state equation based on the optimal estimation
本文中以星敏感器和光纤陀螺为基本配置组成的深空探测器姿态测量系统为对象,针对星敏感器与光纤陀螺联合定姿模式和基于星敏感器的定姿模式,对深空探测器的三轴姿态滤波技术方案进行了设计与研究。