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    • 4. 发明授权
    • Method and apparatus for spoofing of infrared, radar and dual-mode guided missiles
    • 用于伪造红外线,雷达和双模导弹的方法和装置
    • US08223061B2
    • 2012-07-17
    • US11988824
    • 2006-06-28
    • Heinz BannaschMartin Fegg
    • Heinz BannaschMartin Fegg
    • F41J2/00F41J2/02G01S7/38F42B5/15F42B12/70F42B5/00F42B12/00
    • F41J2/02F41H11/02F42B12/66F42B12/70
    • The invention proposes to provide distraction spoofing even on modern infrared, radar and dual-mode guided missiles (4) by production of a decoy chain (20). The chain (20) is formed by a plurality of apparent targets which are switched successively, for example by firing of individual chaff submunitions (2.1-2.5). The deployment takes place before or during the search phase of the missile and can in this case, for example, be carried out using the reverse walk-off principle or at the same time simultaneously or successively and in the form of a pattern. This ensures that the decoys (2.1-2.5) act initially in the greatest selected range zone away from the target (3). The spoofing chain (20) created in this way results in the missile (4) having to carry out a series of time-consuming analysis processes on its way to the target (3).
    • 本发明提出即使在现代的红外线,雷达和双模式导弹(4)上也可以通过生产诱饵链(20)来提供分心欺骗。 链条(20)由多个表观目标形成,例如通过点燃各个壳体子弹药(2.1-2.5)连续切换。 部署在导弹的搜索阶段之前或期间进行,并且在这种情况下,例如可以使用反向离散原理或同时或相继地并且以图案的形式进行。 这确保诱饵(2.1-2.5)最初起作用在远离目标(3)的最大选定范围区域内。 以这种方式创建的欺骗链(20)导致导弹(4)必须在到达目标的路上执行一系列耗时的分析过程(3)。
    • 5. 发明申请
    • Method and Apparatus for Spoofing of Infrared, Radar and Dual-Mode Guided Missiles
    • 红外,雷达和双模导弹导弹的方法和装置
    • US20090251353A1
    • 2009-10-08
    • US11988824
    • 2006-06-28
    • Heinz BannaschMartin Fegg
    • Heinz BannaschMartin Fegg
    • F41J2/02
    • F41J2/02F41H11/02F42B12/66F42B12/70
    • The invention proposes to provide distraction spoofing even on modern infrared, radar and dual-mode guided missiles (4) by production of a decoy chain (20). The chain (20) is formed by a plurality of apparent targets which are switched successively, for example by firing of individual chaff submunitions (2.1-2.5). The deployment takes place before or during the search phase of the missile and can in this case, for example, be carried out using the reverse walk-off principle or at the same time simultaneously or successively and in the form of a pattern. This ensures that the decoys (2.1-2.5) act initially in the greatest selected range zone away from the target (3). The spoofing chain (20) created in this way results in the missile (4) having to carry out a series of time-consuming analysis processes on its way to the target (3).
    • 本发明提出即使在现代的红外线,雷达和双模式导弹(4)上也可以通过生产诱饵链(20)来提供分心欺骗。 链条(20)由多个表观目标形成,例如通过点燃各个壳体子弹药(2.1-2.5)连续切换。 部署在导弹的搜索阶段之前或期间进行,并且在这种情况下,例如可以使用反向离散原理或同时或相继地并且以图案的形式进行。 这确保诱饵(2.1-2.5)最初起作用在远离目标(3)的最大选定范围区域内。 以这种方式创建的欺骗链(20)导致导弹(4)必须在到达目标的路上执行一系列耗时的分析过程(3)。
    • 6. 发明授权
    • Method and apparatus for protecting ships against terminal phase-guided missiles
    • 保护船舶免遭终端导向导弹的方法和装置
    • US07886646B2
    • 2011-02-15
    • US10574532
    • 2004-09-01
    • Heinz BannaschMartin Fegg
    • Heinz BannaschMartin Fegg
    • B64D1/04
    • F41H11/02F41G3/04F41H3/00F41J2/00
    • The present invention concerns a method for protecting ships against terminal phase-guided missiles provided with a target data analysis system, as well as an apparatus for implementing the method, wherein the missile moving in a direction towards the ship to be protected is detected by suitable sensors, located, and its expected trajectory is calculated by a computer; the type of target data analysis performed by the missile and its attack structure is detected by suitable sensors, and the missile is classified with regard to the type of its target data analysis; the current wind speed and direction of wind is continuously detected by wind measuring sensors; the ship's own data: travelling speed, direction of travel, rolling and pitching motions, is continuously detected by motion and/or navigation sensors; the detected sensor data is transmitted to a fire control calculator which controls at least one decoy launcher and generates, by taking into account all of the detected data, an effective decoy pattern that is adapted to missile and attack structure.
    • 本发明涉及一种用于保护船舶抵御设有目标数据分析系统的终端相位导弹的方法,以及用于实施该方法的装置,其中,朝向被保护船舶的方向移动的导弹通过适当的 传感器位于,其预期轨迹由计算机计算; 通过适当的传感器检测导弹及其攻击结构进行的目标数据分析的类型,并根据目标数据分析的类型对导弹进行分类; 当前的风速和风向由风测传感器连续检测; 运动和/或导航传感器连续检测船舶自身的数据:行驶速度,行驶方向,滚动和俯仰运动; 检测到的传感器数据被发送到控制至少一个诱饵发射器的火灾控制计算器,并且通过考虑所有检测到的数据,生成适于导弹和攻击结构的有效诱饵图案。
    • 7. 发明申请
    • Method and apparatus for protecting ships against terminal homing phase-guided missiles
    • 保护船舶抵御终端导向相导弹的方法和装置
    • US20070159379A1
    • 2007-07-12
    • US10574532
    • 2004-09-01
    • Heinz BannaschMartin Fegg
    • Heinz BannaschMartin Fegg
    • G01S13/00
    • F41H11/02F41G3/04F41H3/00F41J2/00
    • The present invention concerns a method for protecting ships against terminal homing phase-guided missiles provided with a target data analysis system, as well as an apparatus for implementing the method, wherein the missile moving in a direction towards the ship to be protected is detected by suitable sensors, located, and its expected trajectory is calculated by means of a computer; the type of target data analysis performed by the missile and its attack structure is detected by means of suitable sensors, and the missile is classified with regard to the type of its target data analysis; the current wind speed and direction of wind is continuously detected by means of wind measuring sensors; the ship's own data: travelling speed, direction of travel, rolling and pitching motions, is continuously detected by means of motion and/or navigation sensors; the detected sensor data is transmitted to a fire control calculator which controls at least one decoy launcher and generates, by taking into account all of the detected data, an effective decoy pattern that is adapted to missile and attack structure.
    • 本发明涉及一种用于保护船舶对具有目标数据分析系统的终端归巢相位导弹的保护方法,以及用于实施该方法的装置,其中,朝向待保护船舶的方向移动的导弹通过 通过计算机计算位于其中的合适的传感器及其预期轨迹; 通过适当的传感器检测导弹及其攻击结构进行目标数据分析的类型,并根据目标数据分析的类型对导弹进行分类; 目前的风速和风向是通过风力传感器连续检测的; 通过运动和/或导航传感器连续检测船舶自身的数据:行驶速度,行驶方向,滚动和俯仰运动; 检测到的传感器数据被发送到控制至少一个诱饵发射器的火灾控制计算器,并且通过考虑所有检测到的数据,生成适于导弹和攻击结构的有效诱饵图案。
    • 8. 发明授权
    • Method for offering a phantom target, and decoy
    • 提供幻影目标的方法和诱饵
    • US06513438B1
    • 2003-02-04
    • US09697160
    • 2000-10-27
    • Martin FeggHeinz Bannasch
    • Martin FeggHeinz Bannasch
    • F42B426
    • F42B12/70F41H11/02H01Q15/14
    • A method and associated decoy for offering a phantom target for protecting land, air or water vehicles or the like as a defense against missiles possessing a target seeking head operating in the infrared (IR) or radar (RF) range, or a target seeking head simultaneously or serially operating in both wavelength ranges. An effective mass emitting radiation in the IR range (IR effective mass) based on flares and a mass backscattering RF radiation (RF effective mass) based on dipoles are simultaneously made to take effect in an appropriate position as a phantom target. A ratio of dipole mass to flare mass of approx. 3.4:1 to approx. 6:1 is employed; and flares presenting a descent rate approx. 0.5 to 1.5 m/s higher than that of the dipoles are used.
    • 一种用于提供用于保护陆地,空中或水上车辆等的幻影目标的方法和相关联的诱饵,以防止具有在红外(IR)或雷达(RF)范围内操作的目标寻求头的导弹,或目标寻求头 在两个波长范围内同时或连续工作。 基于耀斑的红外范围(IR有效质量)和基于偶极子的质量反向散射RF辐射(RF有效质量)的有效发射辐射同时作为体模目标在适当的位置生效。 偶极质量与耀斑质量之比约为 3.4:1〜 6:1; 并且发射速率约为。 使用比偶极子高0.5〜1.5m / s。