您要查找的是不是：
- Strapdown inertial guidance system 捷联惯性制导系统
- The Application of DSP in Strapdown Inertial Guidance System DSP在捷联惯性制导技术中的应用
- Auto-alignment Method for Strapdown Inertial Guidance Missile 捷联惯性制导导弹自对准方法
- Study on Redundant Technology in the Strapdown Inertial Guidance System 冗余技术在捷联惯导系统中的应用研究
- Strapdown Inertial Guidance System Consi sting of Piezoelectric Inertial Sensors 压电捷联惯导系统研究
- Flight test analysis of an improved transfer alignment for missile strapdown inertial guidance system 弹载捷联惯性制导系统传递对准技术试飞验证
- METHOD OF INITIAL ALIGNMENTS OF A SHORT RANGE MISSILE WITH STRAPDOWN INERTIAL GUIDANCE SYSTEM 近程导弹捷联惯导系统初始对准方法与误差模型
- The Experiment and Simulation Research of Initial Alignment of the Strapdown Inertial Guidance System of Short Range Missile 近程导弹捷联惯导初始对准试验与仿真研究
- strapdown inertial guidance 捷联式惯性制导
- Chen Zhe. Strapdown inertial navigation systerm theory [ M ]. 陈哲.;捷联惯性导航系统原理[M]
- It is an effective way in integrated navigation by using Strapdown Inertial Navigation System(SINS),GPS and Doppler Velocity Log(DVL). 利用捷联惯导(SINS)、GPS定位系统和多普勒计程仪(DVL)进行组合导航是水下运载器导航定位的有效方式。
- An independently integrated navigation system using odometer (OD) to assist the strapdown inertial navigation system (SINS/OD) is discussed. 摘要利用里程计辅助捷联惯导系统构成一种完全自主式的车载组合导航系统。
- The moving base initial alignment for GPS-aided RLG Strapdown Inertial Navigation Systems is introduced in this paper. 对GPS辅助下的激光陀螺捷联惯导系统的动基座初始对准进行了实验研究。
- The closed-loop interference fiber optic gyroscopes and strapdown inertial measurement unit are introduced. 介绍了闭环方案的干涉型光纤陀螺仪和捷联惯性测量组合。
- Inertial guidance is often used in medium and long range missiles (over 40km say) when the intention is to hit a given map reference. 中远程导弹（比如说超过40公里）要想命中某一个给定的目标，经常采用惯性制导。
- Error Analysis and Simulation of Ring Laser Gyro Strapdown Inertial Navigation System[J]. 引用该论文 吉翠萍;陈勇;雷宏杰;韩宗虎;陈林峰.
- Firstly, during its flight, the cruise missile “knows” how far and where it has traveled through its IGS (Inertial Guidance System). 首先，在飞行过程中，巡航导弹通过惯性制导系统“知道”它已经飞过多远和已经飞到哪了。
- Myeong-Jong Yu.Equivalent error models of strapdown inertial navigation system[M].AIAA 297-3563. 谷宏强;马立元;郭利.;速率捷联惯性测量系统的数学模型及误差标定[J]
- Based on the inertial guidance instrument error model,the model of reentry point's parameters is established in this paper. 基于惯性制导工具误差模型,推导出存在工具误差时的再入点运动参数模型。
- The initial alignment and calibration of strapdown inertial system on a rocking base are investigated. 研究摇摆基座上捷联惯性导航系统的初始对准技术。
