terminal accuracy

Analysis of the Synthetic Factors Affecting the Hit Accuracy of the Semi-active Laser Terminal Detection and Trajectory Impulse Correction Projectile

影响末段脉冲修正弹命中精度的综合因素分析

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Individual inductor connected between the inverter ′ s output terminal and the load can restrain the circulating-current well with the disadvantage of reducing the steady-state voltage accuracy of parallel system.

在逆变器输出端串联电感能够较好地抑制并联逆变器模块间环流，其缺点是降低了并联系统的稳态电压精度。

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The terminal guidance accuracy assessment is an important aspect of weapon system appraisement in tactical and technical capability, which has always been drawn attention from the design and test department, and the users.

武器系统末端导引的精度评估是评价武器系统战技性能的重要环节，历来受到设计、试验和使用部门的关注。

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Nowadays, the shoot data of ship to ship missile only ensures the accuracy of self control terminal without parameter control of missile trajectory. Based on this situation, a concept on trajectory planning was raised.

根据当前飞航式反舰导弹的射击诸元只精确确定导弹的自控终点，而导弹的弹道尚未进行参数控制的现状，提出了弹道规划的基本概念。

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In the past few years, to improve the accuracy of the terminal guidance system, the performance analysis and index distribution of the homing TGS have been paid more and more attention.

近年来，为了进一步提高末制导精度，寻的末制导系统的性能综合分析及指标分配工作越来越受到广泛的重视。

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Relative to the rocker arm type structure, the structure of the target is the same as the simulation target can provide more reasonable and accurate simulation target for laser communication terminal tracking accuracy detection.

相对于摇臂式结构，该靶标的结构形式与被模拟目标相同，能为激光通信光端机跟踪精度测试提供更加合理、准确的模拟目标。

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Numerical simulations show that the spacecraft with the symplectic guidance algorithm can follow the reference orbit precisely under the deterministic velocity errors or the random velocity errors, and obtain the satisfying terminal control accuracy.

结果表明：无论确定性速度误差还是随机速度误差，实时制导保辛算法能够保证航天器很好地跟踪标称参考轨道并达到满意的终端控制精度。

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Research on Covariance Method of Accuracy Analysis in Missile Terminal Guidance

导弹末制导精度分析的协方差方法研究

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The effect of main delay in guidance& control system of interceptor on guidance accuracy is investigated during terminal phase of intercepting a tactical ballistic missile ( TBM).

针对拦截弹在末制导段拦截战术弹道导弹（TBM），本文分析了拦截弹制导控制系统中存在的导引头信息处理延迟、制导控制指令延迟和执行机构响应延迟对制导精度的影响。

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Furthermore, a guidance law is proposed by using a combination of optimal guidance law design with ideal velocity curve approach. The terminal guidance accuracy, the direction and amplitude of the aerocraft velocity are guaranteed by using the derivative guidance law.

同时采用最优制导律设计与理想速度曲线相结合的方法，设计了能同时保证末端制导精度及速度方向、大小的制导律。

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Major objectives are to improve power system stability and to guarantee generator terminal regulation accuracy. In this paper, based on nonlinear optimal predictive ( NOPC) theory, a novel multi-objective excitation controller with closed-form analytic solution control law is presented.

以提高电力系统稳定性和维持机端压电静态调节精度为目标，基于非线性最优预测控制理论，首次设计出具有闭合的解析形式控制律的非线性励磁控制器。

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The effect of seeker performance on guidance accuracy for using hit-to-kill technology to intercept tactical ballistic missile ( TBM) during terminal phase is investigated.

针对末制导段采用直接碰撞动能杀伤技术的拦截弹拦截战术弹道导弹（TBM），分析了导引头分辨率、帧频和测量噪声等主要性能参数对制导精度的影响。

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