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红外末
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  infrared seekers
     The General Dynamics/ Westinghouse's AAAM concept uses folded long-chord cruciform wings and narrow-chord cruciform tailfins, a tandem-rocket booster plus a sustainer rocket with thrust-vector control, inertial midcourse guidance system plus semi-active radar / infrared seekers.
     通用动力-西屋公司的方案采用可折叠的长弦十字形弹翼和窄弦十字形尾翼,串列式助推器加上火箭主发动机,惯导加半主动雷达/红外末制导,并采用了推力向量控制系统。
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  “红外末”译为未确定词的双语例句
     The state estimation about infrared terminal guidance for space intercept
     空间拦截红外末制导中的状态估计
短句来源
     Infrared Terminal-Guidance of Phase-Controlling Super-Speed Target Detection Technology
     相控红外末制导高速目标检测技术
短句来源
     ESTIMATION OF THE RANGE BETWEEN THE INTERCEPTER AND THE TARGET DURING INFRARED TERMINAL GUIDANCE OF SPACE INTERCEPTION
     空间拦截红外末制导中拦截器与目标相对距离的估计
短句来源
     Study on Aero-optical Effect in the Terminal Infrared Guidance
     红外末制导中的气动光学效应分析
短句来源
     A proper mathematical model is built according to the kinematic equations of space interception. After the component of the relative velocity normal to the line of sight is observed using a nonlinear observer design method with two canonical forms, the problem of estimating the range between the intercepter and the target during infrared terminal guidance of space interception is solved.
     从空间拦截运动学方程出发建立了一个恰当的数学模型,运用基于两种规范型的非线性状态观测器设计方法,通过对相对速度在视线法向分量的观测,解决了红外末制导中拦截器与目标相对距离的估计问题。
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  相似匹配句对
     SIGNAL PROCESSOR DESIGN FOR INFRARED IMAGING TERMINAL GUIDANCE
     红外成像制导处理机设计
短句来源
     Study on Aero-optical Effect in the Terminal Infrared Guidance
     红外制导中的气动光学效应分析
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     Infrared Therapy
     红外医疗
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     The Infrared Measuring Technology for Temperature
     红外测温技术
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     Last Weekend
     上周
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This article describes development of US' Advanced Air-to-Air Missile and concepts proposed by two industrial teams. The General Dynamics/ Westinghouse's AAAM concept uses folded long-chord cruciform wings and narrow-chord cruciform tailfins, a tandem-rocket booster plus a sustainer rocket with thrust-vector control, inertial midcourse guidance system plus semi-active radar / infrared seekers. The Hughes / Raytheon's missile uses a single pair of wings, a integral rocket / ramjet propulsion systems, and active...

This article describes development of US' Advanced Air-to-Air Missile and concepts proposed by two industrial teams. The General Dynamics/ Westinghouse's AAAM concept uses folded long-chord cruciform wings and narrow-chord cruciform tailfins, a tandem-rocket booster plus a sustainer rocket with thrust-vector control, inertial midcourse guidance system plus semi-active radar / infrared seekers. The Hughes / Raytheon's missile uses a single pair of wings, a integral rocket / ramjet propulsion systems, and active radar / imaging-infrared guidance. The two concepts are in the competition.

本文介绍了美国先进空空导弹(AAAM)研制情况及两个工业小组提出的AAAM导弹方案。通用动力-西屋公司的方案采用可折叠的长弦十字形弹翼和窄弦十字形尾翼,串列式助推器加上火箭主发动机,惯导加半主动雷达/红外末制导,并采用了推力向量控制系统。休斯-雷锡恩公司的方案采用单对弹翼,整体式火箭-冲压发动机,主功雷达和光电结合的制导方式。这两种方案正在竞争之中。

The design method for nonlinear state observer based on two kinds of standardization design method is introduced in this paper, the relative range between the intercepter and the target during infrared terminal guidance for space intercept is estimated by the method.The results of simulation verify that the above method is effective.

本文首先简要地介绍了基于两种规范型的非线性状态观测器的设计方法,然后用该法解决了空间拦截红外末制导中拦截器与目标相对距离的估计问题,仿真结果表明估计的效果良好。

A proper mathematical model is built according to the kinematic equations of space interception. After the component of the relative velocity normal to the line of sight is observed using a nonlinear observer design method with two canonical forms, the problem of estimating the range between the intercepter and the target during infrared terminal guidance of space interception is solved. The numerical simulation verifies the above results.

从空间拦截运动学方程出发建立了一个恰当的数学模型,运用基于两种规范型的非线性状态观测器设计方法,通过对相对速度在视线法向分量的观测,解决了红外末制导中拦截器与目标相对距离的估计问题。仿真结果表明估计的效果良好

 
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