传递对准是现代惯性制导武器的关键技术。
Transfer alignment is one of the key techniques in modern inertial guidance weapons.
制导由配有卫星导航的惯性制导打包提供。
Guidance is provided by an inertial package coupled with satellite navigation.
得益于俄罗斯技术，搜索器和惯性制导系统由莫斯科提供。
The PL-12 does benefit from Russian technology, with the seeker and inertial guidance system provided by Moscow.
本文导出了惯性制导工程中广泛应用的摄动方程转移矩阵的解析解。
The transition matrix analytic solution of perturbation equations which was widely used in inertial guidance engineering are derived.
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。
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。
This paper proposes a nonlinear model for guidance instrument systematic error separation based on tracking trajectory data.
弹道模型由炮弹无控自由飞段、惯性制导滑翔段和末制导段按比例导引制导率建立。
The trajectory model consists of the uncontrolled free flight segment, the inertial guided glided segment and the final guidance segment, which accords with the proportional guided law.
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。
The paper introduces a very low cost strapdown inertial guidance system consisting of piezoelectric gyros and low cost accelerometers.
火箭的飞行相比以前要快得多，而且它仅需要几分钟的惯性制导就能把武器推送到一个可预测的弹道路径上。
Rockets flew much faster and required inertial guidance for just a few minutes to put the weapon on a predictable ballistic path.
结果表明，在发动机点火时间范围内，点火时间对无控弹道射程和惯性制导启控点散布影响不大。
Results show that the rocket ignition time has little effect on uncontrolled trajectory and the dispersion of the starting position of guidance in the range of the rocket ignition time.
双轴平台系列ST 2500是一个高精度位率系统，专为测试及校正陀螺仪、加速表和惯性制导系统。
The dual axis table serie ST 2500 is a high accuracy position rate system designed for the test and calibration of gyros, accelerometers and inertial guidance systems.
双轴平台系列ST 2356是一个高精度位率系统，专为测试及校正陀螺仪、加速表和惯性制导系统。
The dual axis table series st 2356 is a high accuracy position rate system designed for the test and calibration of gyros, accelerometers and inertial guidance systems.
双轴平台系列ST 2400是一个高精度位率系统，专为测试及校正陀螺仪、加速表和惯性制导系统。
The dual axis table serie ST 2400 is a high accuracy position rate system designed for the test and calibration of gyros, accelerometers and inertial guidance systems.
单轴平台系列ST 1100是一个高精度位率系统，其设计宗旨在于测试及校正陀螺仪﹑加速表和惯性制导系统。
The single axis table series ST 1100 is a high accuracy position rate system designed for the test and calibration of gyros, accelerometers and inertial guidance systems.
单轴平台系列rt 1100是一个高精度位率系统，其设计宗旨在于测试及校正MEMS、陀螺仪，加速表和惯性制导系统。
The single axis table series rt 1100 is an accurate position rate system designed for the test and calibration of MEMS, gyros, accelerometers and inertial guidance systems.
在对JDAM系统组成和精度分析的基础上，详细讨论了JDAM系统的卡尔曼滤波器、捷联惯性导航技术、传递对准和GPS辅助惯性制导等技术。
The Kalman filter, SINS technique, transfer alignment and GPS-aided navigation in JDAM system are analyzed based on the system composition and accuracy analysis.
该课题希望通过对MEMS技术和MEMS惯性传感器的研究，研制和设计出一系列能够应用于火箭和导弹制导的MIMU系统。
By the research for MEMS and the MEMS acceleration sensor, This assignment will finish a series of MIMU system, which will be applied to the rocket and the missile guided system.
该算法可用于纯惯性中制导方案设计。
The proposed algorithm can be used in the design of pure inertial midcourse guidance scheme.
提出了应用概率距离测量对多传感器信息进行一致性检验的方法，并将此方法引入到基于多惯性测量组合的总线式导弹制导控制系统中。
The method for consistency check of multisensor data by using the probability distance measuring is presented, and it used in CAN bus missile guidance and control system based on multi-IMU.
数十年来，四元数及其解法成功地应用于捷联惯性导航和制导系统中，成为经典的算法。
Quaternion method, which has been successfully applied to the Strapdown Inertial Navigation and Guidance for tens year, is classical.
研究了系统惯性对制导问题闭合形式解的影响，并获得了解析形式的解。
The effect of inertia of the guidance systems on the closed form solution to guidance problems is investigated and an analytical solution is obtained.
该类飞行器目前仍采用惯性导航为主要的导航手段，中制导采用地形匹配。
Now the main navigation means of such vehicles still adopts inertial navigation, and intermediate navigation adopts terrain contour matching method.
该类飞行器目前仍采用惯性导航为主要的导航手段，中制导采用地形匹配。
Now the main navigation means of such vehicles still adopts inertial navigation, and intermediate navigation adopts terrain contour matching method.
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