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- The Synthetic Discriminant Function (SDF) algorithm and the optical method to realize SDF are reviewed.A new missile terminal guidance system based on SDF correlator is presented. 論述了綜合判別函數（SDF）的基本理論和光學(xué)實(shí)現途徑，提出了一種基于綜合判別相關(guān)器的導彈末制導系統。
- In basic framework of total system,signal stage,isomorphic simulation for centroid chaff countering anti-ship missile terminal guidance radar,models of warship were researched. 在全系統的、信號級的、同構的仿真研究基本框架下,從研究針對反艦導彈末制導雷達的質(zhì)心式箔條干擾的目的出發(fā),對目標艦的有關(guān)模型進(jìn)行了研究。
- Abstract: The Synthetic Discriminant Function (SDF) algorithm and the optical method to realize SDF are reviewed.A new missile terminal guidance system based on SDF correlator is presented. 文摘:論述了綜合判別函數（SDF）的基本理論和光學(xué)實(shí)現途徑，提出了一種基于綜合判別相關(guān)器的導彈末制導系統。
- Missile Terminal Guidance and Control Against Evasive Targets; Master's thesis 導彈終端制導和控制用于對付企圖逃避打擊的目標/碩士論文
- Perspective Analysis of Submillimeter Wave Technology for Missile Terminal Guidance 亞毫米波導彈末制導技術(shù)前景分析
- Realization method of frequency micro adjustment in automatic detection system of missile terminal guidance radar 頻率微調在導彈末制導雷達自動(dòng)檢測系統中的實(shí)現方法
- The matching problem of terminal maneuver and terminal guidance trajectory of anti-ship missile is analyzed. 對反艦導彈的末端機動(dòng)與末制導段彈道之間的配合問(wèn)題進(jìn)行了分析。
- A terminal guidance model is designed for air-to-air missile (AAM)to intercept maneuvering targets in this paper. 構造了攔截加速機動(dòng)目標的空空導彈末制導狀態(tài)模型。
- The final phase is terminal guidance when the missile uses a highly accurate tracking system to make rapid maneuvers for intercepting the target. 最后的階段是末端制導，此階段導彈利用高精度的追蹤系統，快速機動(dòng)，截擊目標。
- In the terminal guidance stage of longrange airtoground missile, its parameters vary widely and abruptly, causing the missile to miss the target. 制導精度分析是空地導彈制導控制系統設計過(guò)程中必須考慮的關(guān)鍵因素之一。
- A simplified linearized feedback control method of terminal guidance was put forward for a nonlinearized model including unknown parameters of missile in this paper. 針對包含未知參數的導彈運動(dòng)非線(xiàn)性模型,提出了一種用于末制導的線(xiàn)性化反饋簡(jiǎn)化控制方法。
- For observing, evaluating and researching the effect of ECM to terminal guidance radar of antiship missile, a simulation system for ECM to antiship missile is developed. 為觀(guān)察、評估和研究針對反艦導彈末制導雷達的電子干擾的效果,研制了一個(gè)反艦導彈電子對抗仿真系統。
- High-speed reentry aerocraft is usually with terminal guidance system. 高速再入飛行器通常具有末制導系統。
- Simulation result showed that response time of missile was reduced and guidance accuracy was accordingly increased by side jet and aerodynamic compound control manner in terminal guidance. 通過(guò)仿真研究表明：在末制導階段，采用燃氣動(dòng)力/氣動(dòng)力復合控制方式可提高導彈的快速性，進(jìn)而提高導彈的制導控制精度。
- The simulation of the terminal guidance procedure is carried out, and some factors which affect the miss distance quantity are analyzed. 提出了修正比例導引律的實(shí)現方案 ,進(jìn)行了末制導過(guò)程的仿真 ,并分析了影響脫靶量的一些因素。
- To improve the capture probability,the hand-over point of anti-ship missiles between midcourse guidance and terminal guidance was analyzed. 為了提高對目標的捕捉概率,研究了反艦導彈中末制導交班點(diǎn)的選擇問(wèn)題。
- Based on the six-freedom-degree ballistic equations, the model of air to ground submunition in the terminal guidance stage was established. 利用六自由度動(dòng)力學(xué)模型對末段彈道進(jìn)行了仿真。
- From the characteristics of terminal guidance projectile at moving targets,the impact conditions of moving targets in simulation system were analyzed. 從末制導炮彈對運動(dòng)目標射擊的特點(diǎn)出發(fā),探索了模擬系統設計中運動(dòng)目標的命中條件。
- From the characteristics of terminal guidance projectile at moving targets, the impact conditions of moving targets in simulation system were analyzed. 摘要從末制導炮彈對運動(dòng)目標射擊的特點(diǎn)出發(fā)，探索了模擬系統設計中運動(dòng)目標的命中條件。
- One simulation system for anti-missile ECM is developed. This system is aimed at anti-ship missiles with terminal guidance radar and may work on a high performance PC. 研制了一個(gè)可以在高性能個(gè)人計算機上運行的、針對采用末制導雷達的反艦導彈的電子對抗問(wèn)題的仿真系統。
