inertial guidance

1. Measurement Error Model of IMU in Strapdown Inertial Guidance System of Manpads Missile
   捷联式惯性导航系统单兵导弹捷联惯导系统IMU测量误差模型
2. Software Design of an Airplane Inertial Guidance System Simulator
   某型飞机惯性导航系统模拟器软件设计
3. 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。
4. In this paper, the passive radar homing combined with the strap down inertial guidance is used on an antiradiation missile to work against the radar stopping radiating.
   本文采用了被动雷达寻的复合惯性末制导做为反辐射导弹的抗雷达关机方案；
5. Radio inertial guidance system
   无线电惯性制导系统
6. Inertial guidance is often used in medium and long range missiles ( over40km 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。
7. In inertial guidance systems, you have a spinning wheel, at least in the days that the guidance systems had mechanical wheels.
   在惯性制导系统中，有一个旋转的轮，至少当制导系统里存在，机械的轮子。
8. This is the basic idea behind inertial guidance systems.
   这是惯性制导系统，的基础概念。
9. Will go from terrain following to inertial guidance.
   会沿地面循着惯性引导。
10. Evaluation model for error compensation of inertial guidance system
    惯性制导系统误差补偿评估模型研究
11. Imtegrated Application of Information of GPS and Inertial Guidance in the Spacecraft Guidance
    GPS和惯导信息在飞行器制导中的综合应用
12. The Methods of Analysis and Evaluation for Errors of Inertial Guidance System in Flight Test
    利用飞行试验数据对惯性制导系统误差进行分析鉴定的方法
13. The precise gravity modeling for inertial guidance
    惯性制导中的精确引力模型
14. On Circuit Design of Strapdown Inertial Guidance System
    捷联惯性制导系统的电路设计
15. The paper introduces a very low cost strapdown inertial guidance system consisting of piezoelectric gyros and low cost accelerometers.
    提出一种低成本捷联惯性制导系统方案。该系统主要由压电陀螺和低成本加速度计构成。
16. The relationship between the output of stellar-tracker and the error angles of inertial guidance platform was deduced.
    导出了星体跟踪器的测量输出与平台误差角之间的数学方程。
17. The testing results in two inertial guidance systems show that the concept is practicable and reliable.
    经过两个型号惯导系统的对准试验，证明该方案具有一定的实用性和可靠性。
18. Modelling method and simulation result by using kalman filter for GPS-INS information processing are described in this paper. Effects of integration of GPS and inertial guidance not only can raise guidance accuracy but also may evaluate guidance error.
    在本文中叙述了利用卡尔曼德波器对GPS、惯导系统信息进行综合的建模方法及仿真结果，说明GPS和惯导组合不但可以提高制导精度，还可估计制导误差。
19. The paper described an improved transfer alignment scheme for missile Inertial Guidance System, and presented the flight test procedure in a transporter.
    介绍了一种弹载捷联式惯性制导系统传递对准改进设计方案，描述了在运输机上进行试飞验证的方法和结果。
20. Inertial guidance system and global positioning system abroad are introduced, and the development of GPS/ INS composite guidance technique which is widely applied to missiles and other weapons is discussed emphatically.
    在分别介绍国外惯性导航系统（INS）和全球定位系统（GPS）的基础上，着重叙述了在导弹和其他武器装备中广泛使用的GPS/INS复合制导技术的发展概况。
21. The Application of DSP in Strapdown Inertial Guidance System
    DSP在捷联惯性制导技术中的应用
22. The first level is passive radar+ infrared ray sensor, the second is strapdown inertial guidance system.
    第一级是被动雷达加红外传感器复合寻的，第二级是一套捷联惯导系统。
23. The auto-alignment for strapdown inertial guidance missile is realized through the method of two-position-zero-torque.
    提出并探讨了采用双位置、零力矩法实现捷联惯性制导导弹自对准的方法。
24. This Paper describes the error propagation properties of IGS ( Inertial Guidance System) for ICBM.
    本文讨论远程弹道导弹惯性制导系统的误差传播特性。
25. 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
26. The results indicate that two-position-zero-torque method can be applicable for the auto-alignment of strapdown inertial guidance missile.
    精确位置转换的方法。研究结果表明，双位置、零力矩法能适用于捷联惯性制导导弹自对准。
27. The hardware of the DSP-based strapdown inertial guidance system is introduced in details.
    讨论了基于DSP的捷联惯导系统的硬件设计，包括基本功能的实现、原理框图及外围电路的设计。
28. Based on the study of the system model in different flight conditions, and by use of real-time compensation in inertial guidance, a method is put forward for selecting the error compensation model and the model of compensation evaluation based on the engineering background.
    通过研究飞行工作环境变化导致的系统模型差异，结合惯性制导实时补偿方法，提出了基于工程背景的误差补偿和补偿评估模型的选取方法。
29. The Application Of PLD In inertial Guidance Test System
    PLD在惯导测试系统中的应用
30. Test table is a kind of important equipment for inertial guidance test.
    测试转台是一种重要的惯导测试设备，它主要是针对陀螺测试和姿态仿真两个目的发展起来的设备。

noun

1. a method of controlling the flight of a missile by devices that respond to inertial forces

   Synonym:    inertial navigation