该电路也是在制导控制系统和导航系统的高性能陀螺仪的使用。
This circuitry is also in use in high-performance gyroscopes in guidance control systems and navigation systems.
从弹道稳定性的要求出发，对制导控制系统相关参数选择的原则给出了定量的结果。
According to the requirement of trajectory stability, the quantitative principle of related parameter choosing is presented.
从弹道稳定性的要求出发，对制导控制系统相关参数选择的原则给出了定量的结果。
According to the requirement of trajectory stability, the quantitative principle of related parameter choosing is advanced.
制导控制系统设计合理，对于静止和机动目标，落点射击精度和落角均满足设计要求。
The guidance and control system is properly designed and can meet the accuracy and attack Angle requirement for still or mobile target.
针对某型导弹控制系统，通过自适应控制理论的应用，介绍了一种自适应制导控制系统的构建方法。
A design method of adaptive flight control system for certain missile control system is introduced in this paper, in which adaptive control theory can be applied.
分析了某类导弹系统的稳定性，研究了天线罩瞄准线误差斜率A的摄动对寻的制导控制系统的影响。
The stability of a kind of missile guidance system is analyzed, and the effect of perturbation of radome boresight error slope a on the stability is investigated.
数字仿真结果表明，所设计的制导控制系统耦合回路对天线罩瞄准线误差斜率的摄动具有较好的鲁棒性。
The digital simulation showed that the coupling loop in guidance control system had satisfactory robustness for the disturbance of error slope for radome's aiming line.
为了实现所设计的方案弹道，提出了制导控制系统的总体方案，建立了滑翔制导炮弹的控制系统数学模型。
In order to realize the designed project trajectory that the guidance and control overall scheme is proposed and control system mathematical model of guided projectile is established.
仿真结果表明，与实际飞行试验数据达到非常好的拟合，说明采用六自由度的制导控制系统的数学模型进行设计的正确性。
Numerical simulation results for sample engagement scenarios are given. It shows that simulation results are very close to the actual flight test results. So …
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.
增强型寻的器将每个SCALPEL精确导引至目标，先进制导与控制系统持续演示其精确度。
The enhanced seeker accurately guided each SCALPEL to its target, and the advanced guidance and control system consistently demonstrated its precision.
仿真结果表明，设计的自动控制系统能够使滑翔制导炮弹在飞行过程中具有良好的响应特性，方法简单，易于实现。
The simulation results show that the automatic control system can make the guided projectile response perfectly and design method is simple and achieved easily.
质量是一个永恒问题，更是军工产品的生命线，也是导航、制导与控制系统研制和生产中所存在的一个关键问题。
Quality is a permanent problem. It is not only a lifeline of military products, but also a key problem of research and production in navigation, guidance and control system domain.
复合控制采用对制导指令进行前向分解的方法，将复合控制系统分为两个并行的子系统，即气动力控制子系统和直接力控制子系统。
By means of guidance command decomposed forwardly, the combined control system is divided into two parallel subsystems: the aerodynamics subsystem and the direct force subsystem.
针对目前制导炸弹命中精度低的问题，提出一种基于自适应神经模糊推理系统(ANFIS)的制导炸弹智能控制系统。
Aiming at the problem of guided bombs in low precision, this paper presents a kind of intelligence control system of guided bomb based on Adaptive Neuro-Fuzzy Inference system (ANFIS).
选择自动驾驶仪制导体制，建立了机载布撒器纵向控制系统模型。
According to the autopilot guide method, a longitudinal system control model for the air borne dispenser has been built.
总结了国内外在人眼视觉系统方面的研究现状及本课题组对于仿生技术在导弹制导、控制系统中的应用研究的主要内容、已取得的成果以及研究成果的应用前景。
Actuality research station in-out country and production of our team in guidance of missile and control system are discussed. At last, application foreground of this investigation is explained.
提出了制导与控制系统控制命令生成方法。
The method for generating the guidance and control command is presented.
首先，分析了原有激光驾束制导系统，引入了控制系统的改进原则。
Beam rider guidance system was first analyzed, and control system improvement principles introduced.
首先，分析了原有激光驾束制导系统，引入了控制系统的改进原则。
Beam rider guidance system was first analyzed, and control system improvement principles introduced.
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