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- Zero effort miss distance 零效脱靶量
- A midcourse guidance law based on zero effort miss forecasting is presented for intercepting a high-speed target in three-dimensional space. 针对三维空间内的高速飞行目标,提出了一种基于预测零控脱靶量的中制导段导引方法。
- A robust midcourse guidance law based on the zero effort miss is designed for the middle flying stage of exo-atmospheric intercept with the fuel-exhaustion-shutoff solid engine. 摘要针对大气层外拦截中段采用耗尽关机固体燃料发动机的情况，设计了基于零控脱靶量的鲁棒中制导律。
- Midcourse Guidance Based on Zero Effort Miss for Exo-Atmospheric Intercept 基于零控脱靶量的大气层外拦截中制导研究
- zero effort miss 零控脱靶量
- Test error for the miss distance is analyzed and analysis result is given. 分析了脱靶量的测量误差,并给出了分析结果;
- Measurement of miss distance for targets with known modes of motion is studied. 研究运动规律已知的目标脱靶量测量问题.
- An analysis of results in various miss distance and miss azimuth was made. 分析了不同脱靶角和不同脱靶量弹目交会信号;
- Forget all the "get slim quick" schemes out there promising you quick results with zero effort! 忘记"得到快速瘦身计划"出有为有你见效快零努力!
- A way to measuring the miss distance vector by doppler radar theory is described. 描述了一种利用多普勒雷达原理进行脱靶矢量测量的方法。
- Miss distance data processing method is introduced in combination with actual range application. 结合实际靶场应用介绍了脱靶量数据处理方法;
- A way to measuring the vector miss distance using echo signal from Multiple Frequency CW-Tracking Radar is described in this paper. 本文详细介绍了利用多频连续波测量雷达回波信号进行脱靶量测量的方法。
- The simulation of the terminal guidance procedure is carried out, and some factors which affect the miss distance quantity are analyzed. 提出了修正比例导引律的实现方案 ,进行了末制导过程的仿真 ,并分析了影响脱靶量的一些因素。
- In this paper, the control law of DACS is investigated, and miss distance simulation model of intercepting TBM is established. 本文探讨了动能拦截器在末制导段拦截战术弹道导弹的轨道和姿态控制规律,建立了拦截的脱靶量仿真数学模型。
- In this paper,the miss distance measurement problem for targets in rectilinear motion and with constant accelerations is studied. 本文研究了匀加速直线运动目标的脱靶量测量问题 .
- Miss distance is an important data in aircraft survivability evaluation and the main criterion to infrared decoy efficiency. 脱靶距离是飞机生存力评估的重要数据,红外诱饵弹对红外制导导弹的干扰效果也可通过脱靶距离来衡量。
- Miss distance parameters are estimated by matching pursuit algorithm to search the basis function which best matches the echo signal. 通过匹配追踪算法寻找与回波信号最匹配的基函数来确定脱靶量参数。
- The miss distance caused by guidance method error and the effects of perturbation are compensated in this initial guidance law. 该初制导方法能补偿制导方法误差和轨道摄动对拦截脱靶量的影响。
- So in actual design, guidance system time constant should match the TADS frequency bandwidth to avoid large miss distance. 因此在实际设计中，应匹配具体制导系统的时间常数和稳瞄系统的频带，以避免产生较大脱靶量。
- Based on the attributes of different errors, the method for transferring miss distance measurement error in servo control system is given. 在考虑不同误差属性的基础上，给出了脱靶量测量误差在伺服控制系统中的传递方法。
