An inertial controlling scheme to the altitude with the signal of the axis apparent velocity and its integral by the method of conjugate equation is presented in this paper.
本文以飞行器轴向视速度及其积分为控制信号，用共扼方程法设计了一种惯性高度控制方案。
2
The outputs of these accelerometers are the three coordinates of the inertialvelocity of the vehicle with the exception of gravity effects.
这些加速度计的输出是三个没有重力影响的飞行器惯性速度座标。
3
Active Radar Seeker (ARS) provides accurate and stable velocity information, thus possesses the possibility of gimbaled inertial navigation system (GINS) aiding.