Fos paper completes softwar design of the navigation system based on vxworks 本文完成了新一代基于实时操作系统的平台式惯性导航系统的总体软件设计。
3 . the aim of initial alignment of sins is to compute the initial values of strapdown matrix 捷联惯性导航系统初始对准的目的是建立捷联矩阵的初始值。
This paper were analyze the characteristic of the drift and discuss the compensation methods for it 为了把ifog应用于惯性导航领域，必须改善其漂移特性。
The airborne inertial navigation system is the part which may not be lacked in the aviation electronics 机载惯性导航系统是航空电子设备中不可或缺的部分。
Inertial navigation is essentially to solve the kinematic problem of a three - dimensional rigid body 惯性导航本质上要解决的是一个三维空间的刚体运动学问题。
3 . error characteristics of the strapdown inertial navigation are investigated using dual quaternion 3 .运用对偶四元数代数研究了捷联式惯性导航的误差特性。
The flight control system contains gps & ins , which insured auto takeoff & landing , as well as the whole flight process 飞行控制系统采用gps全球定位系统和惯性导航系统，可自动完成从起飞到着陆的整个飞行过程。
The first half of this thesis has done some pilot works on the strapdown inertial navigation theory founded on dual quaternion 论文的前半部分在建立基于对偶四元数的捷联惯性导航系统理论方面作了一些探索性工作。
Gyroscope is indispensable in the control systems and inertial navigation systems on the carriers , such as the plane , the missile , the ship ect 陀螺仪是飞机、导弹、舰船等运载体及惯性导航系统不可缺少的重要元件。
Finally , combining algorithm flow - chart of the sins , all work realizes test and validation of the hardware circuit system 最后，结合捷联式惯性导航系统算法流程，对硬件电路系统进行了测试验证，并给出了测试结果。
