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   飞机突防 的翻译结果: 查询用时:0.273秒
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飞机突防
相关语句
  airplane penetration
     Key Techniques for Airplane Penetration in Round Attacking Planning
     飞机突防波次规划中若干关键技术研究
短句来源
  aircraft penetration
     Real-Time Simulation Implementation of Nonlinear Decoupling Control for Aircraft Penetration Flight
     飞机突防飞行非线性解耦控制的实时仿真实现
短句来源
     A HYBRID SIMULATION STUDY OF NONLINEAR DECOUPLING CONTROL SYSTEM FOR AIRCRAFT PENETRATION
     飞机突防飞行非线性解耦控制系统的混合仿真研究
短句来源
     NONLINEAR DECOUPLING CAPTURING OF AIRCRAFT PENETRATION TRAJECTORY
     飞机突防航迹的非线性解耦跟踪
短句来源
     THE DECISION OF AIRCRAFT PENETRATION ROUTE THROUGH HOSTILE DEFENCE AREA
     防御区域飞机突防航迹的决策
短句来源
     WORST-CASE WIND MODELING AND ITS INFLUENCE ON CAPTURING OF AIRCRAFT PENETRATION TRAJECTORY
     最坏风模型及对飞机突防航迹跟踪的影响
短句来源
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  “飞机突防”译为未确定词的双语例句
     The effect of turbulent disturbance on the behavior of decoupling control in case of an aircraft penetrating at low level by using TF/TA technologies and control and its riding quality of the pilot are studied by pilot-vehicle semi-physical simulation technique. At the same time, the tracking behavior of nonlinear decoupling system on the real-time control command of the pilot is verified,too.
     本文利用人机半物理仿真法,研究了大气紊流对飞机突防飞行的解耦控制特性、驾驶员的操纵性及乘坐品质的影响,检验了非线性解耦控制系统对驾驶员实时操纵指令的跟踪特性。
短句来源
     In this paper, architecture of weapon countermine simulation system based on HLA is introduced,and followed by a discussion of the development process of HLA-based simulation applications. Finally,in a case study of Air-Ground combat simulation,this paper introduces and analyses the development process and mothod of weapon countermine simulation system.
     该文首先介绍了基于HLA的武器对抗仿真系统的结构 ,然后介绍了基于HLA的仿真应用系统的开发过程 ,最后 ,以飞机突防作战仿真为例 ,从应用的角度分析了基于HLA的武器对抗仿真系统开发过程和方法 ;
短句来源
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  aircraft penetration
Improved methods are required for operationally estimating storm structure and strength when aircraft penetration is not possible.
      


Based on a kind of non-linear dynamic equations,the differecntial game solutions of quadratic payoff function are developed,so the worst-case wind models contatining non-inear factors are constructed.This model especially pertains to analyse disturbance sensitivity problem of aircraft during spatial maneurering flight.Finally,how the non-linear decoupling ccapturing of aircraft penetration trajectory is affected by this variable wind field is discussed.

针对一类非线性动力学系统,本文推导出二次型性能指标下的微分对策解,由此得到一组含有非线性因素的最环风模型,这一模型特别适用于研究作空间机动飞行的飞机受外界环境扰动的灵敏性问题。最后考察了这一变化风场对飞机突防航迹非线性解耦跟踪的影响。

The effect of turbulent disturbance on the behavior of decoupling control in case of an aircraft penetrating at low level by using TF/TA technologies and control and its riding quality of the pilot are studied by pilot-vehicle semi-physical simulation technique. At the same time, the tracking behavior of nonlinear decoupling system on the real-time control command of the pilot is verified,too. The simulation results show that some nonlinear cross couple between longitudinal and lateral movements of the aircraft...

The effect of turbulent disturbance on the behavior of decoupling control in case of an aircraft penetrating at low level by using TF/TA technologies and control and its riding quality of the pilot are studied by pilot-vehicle semi-physical simulation technique. At the same time, the tracking behavior of nonlinear decoupling system on the real-time control command of the pilot is verified,too. The simulation results show that some nonlinear cross couple between longitudinal and lateral movements of the aircraft can be eliminated by the decoupling control law, and it offers better decoupling control and riding quality of the pilot. The work load of the pilot could be reduced greatly, and the result of research theory is verified, too.

本文利用人机半物理仿真法,研究了大气紊流对飞机突防飞行的解耦控制特性、驾驶员的操纵性及乘坐品质的影响,检验了非线性解耦控制系统对驾驶员实时操纵指令的跟踪特性。结果表明:解耦控制律能够在大气紊流扰动下解除飞机纵横向运动的非线性交叉耦合,_有良好的解耦操纵性能和乘坐品质,减轻了驾驶员的操纵负担,从而提高了低空突防飞行的安全性,也验证了理论研究的结果

With the view to aircraft penetration flight mission planning,detection space of early warning radar which detects different radar cross section(RCS)of targets at different physiognomy and in different detection probability is generated by critical RCS method,with the following factors being taken into account:curvature of the earth,reflection and clutter interference of land or sea,atmospheric refraction,atmospheric loss,and so on. The influence of flight height,target RCS,detection probability and physiognomy...

With the view to aircraft penetration flight mission planning,detection space of early warning radar which detects different radar cross section(RCS)of targets at different physiognomy and in different detection probability is generated by critical RCS method,with the following factors being taken into account:curvature of the earth,reflection and clutter interference of land or sea,atmospheric refraction,atmospheric loss,and so on. The influence of flight height,target RCS,detection probability and physiognomy on the radar detection space is calculated and analyzed in order to select a low detection probability flight corridor. It is of practical significance to draw up and implement safe penetration flight strategy.

飞机突防飞行任务规划出发 ,综合考虑地球曲率、陆地 (或海洋 )的反射和杂波干扰、大气折射和吸收损耗等因素的影响 ,采用临界散射截面法生成了对空警戒雷达在不同地貌、发现概率下 ,对不同雷达散射截面的目标的探测空间。计算并分析了飞行高度、目标雷达散射截面、发现概率和地貌等因素对雷达探测空间的影响 ,以便选择低探测概率的飞行走廊 ,这对制定和实施安全突防飞行策略有实际意义。

 
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