| 1. | And analyse the deviation of initial alignment
同时,对系统初始对准的误差进行了分析。 |
| 2. | The study of launch vehicle platform align emulation system
运载火箭初始对准仿真系统的研究 |
| 3. | 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。 |
| 4. | But , because of the limitation of imu ' s accuracy , it is impossible to finish its alignment by itself
但是，低成本惯性元件精度低，无法进行自主初始对准。 |
| 5. | Firstly the key technologies about initial alignment and attitude matrix algorithms are systematically discussed
首先对实现sins的初始对准及姿态矩阵计算等关键技术进行了系统研究。 |
| 6. | The thesis contributes to decrease system errors , increase the precision and reliability of alignment .
而且，本文讨论了在初始对准过程中进行测漂的问题，这对于提高系统的精度有很大的帮助。 |
| 7. | The kernel problem of antenna stabilization and tracking technology is the initial alignment and automatic tracking technology of antenna toward satellite
天线稳定跟踪技术的核心问题是天线对卫星的初始对准和自动跟踪技术。 |
| 8. | Two applications of gyro were involved in this paper : one is application in north - seeking system , the other one is research of alignment in sins
本文中涉及到他的两种应用：在找北系统中的应用以及在捷联系统中初始对准的研究。 |
| 9. | Abstract : physical and mathematical model for the inertial platform initialization align system of launch vehicle is discussed in this paper
文摘:本文讨论并建立了运载火箭初始对准系统的物理数学模型，并用多媒体手段对系统实际工作过程进行了仿真模拟。 |
| 10. | This paper was designed from the point of view of control to study sins initial alignment , hammer at to get a better strapdown system initial alignment method
本论文主要是从控制角度出发来研究捷联惯导系统的初始对准问题，力求获得高精度，高可靠性的初始对准方法。 |
