Study on the Simulation of the Attacking Ability for Air to Air Missile

机译：空空导弹攻击能力仿真研究

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Base on the analysis of the characteristics of supersonic speed and maneuver targets and some assumptions, a general model of long-distance air to air missiles attacking supersonic speed and maneuver targets is presented. Begin with various corresponding coordinate systems, the target aircraft model, the long-distance air to air missile model, the moving model of the attacking aircraft and the guide model of long-distance air to air missile are built. Base on the models built and the expanded proportion guide algorithm and make use of the theory of optimal control the optimum guide algorithm is found out. The simulating result shows that the long- distance air to air missiles really have the air defense ability in common fighting height, speed and middle-and-long distance.

机译：在分析超音速和机动目标的特点及一些假设的基础上，提出了攻击超音速和机动目标的长距离空空导弹的通用模型。从各种相应的坐标系开始，建立目标飞机模型，长距离空空导弹模型，攻击机的运动模型以及长距离空空导弹的引导模型。在建立模型和扩展比例指导算法的基础上，利用最优控制理论，找到了最优指导算法。仿真结果表明，长距离空空导弹在共同的战斗高度，速度和中远距离上确实具有防空能力。

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来源
《国际导航制导控制学术会议论文集》||371-376|共6页
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作者
Douglas A.Johnson; rnSodnomdarjaa Jigjidsuren; rnAnlin Gu;
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作者单位

Ju Chuanwen@Naval Aeronautical Engineering Academy, Qingdao Branch QingDao 266041,China--Yang Xiuzhen@Naval Aeronautical Engineering Academy, Qingdao Branch QingDao 266041,China--;

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原文格式 PDF
正文语种 eng;chi
中图分类导航术;
关键词
Supersonic Speed and Maneuver Target; Long-distance Air to Air Missile; Beyond visual range;

机译：超音速速度和机动目标；长距离空空导弹；超视距;

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专利

1. Trajectory Defense of an Aircraft against Air-to-Air Missiles that Attack from the Front Hemisphere [J] . M. A. Demkin, B. E. Fedunov, A. D. Sharaborov Journal of Computer and Systems Sciences International . 2004,第4期

机译：飞机对从前半球进攻的空空导弹的轨迹防御
2. Trajectory defense of an aircraft against air-to-air missiles that attack from the front hemisphere [J] . Demkin MA, Fedunov BE, Sharaborov AD Journal of Computer and Systems Sciences International . 2004,第4期

机译：飞机对前半球攻击的空空导弹的轨迹防御
3. Geometrical approach-based defense-missile intercept guidance for aircraft protection against missile attack [J] . T Yamasaki, S N Balakrishnan, H Takano Proceedings of the Institution of Mechanical Engineers . 2012,第G8期

机译：基于几何进近的防御-导弹拦截指导，用于飞机防御导弹攻击
4. Study on the Simulation of the Attacking Ability for Air to Air Missile [C] . Ju Chuanwen, Yang Xiuzhen ICNGC2001 : International conference on navigation, guidance and control 2001 . 2001

机译：空空导弹攻击能力仿真研究
5. A Quantitative Study Examining United States Passenger Perceptions of the Use of Air Missile Defensive Systems by Civilian Airlines and Potential Impact to the Airline. [D] . Garvin, John D. 2017

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7. Dynamic attack zone of air-to-air missile after being launched in random wind field [O] . Hui Yaoluo, Nan Ying, Chen Shaodong, 2015

机译：空空导弹在随机风场中发射后的动态攻击区
8. Compensating for Latency Variations in Air-to-Air Missile T&E Using Live Aircraft Linked to a Missile HWIL Simulation [R] . McKee, L. 1998

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Study on the Simulation of the Attacking Ability for Air to Air Missile

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