公开(公告)号：US06252537B1

公开(公告)日：2001-06-26

申请号：US06116501

申请日：1980-01-21

申请人： Gajanan H. Joshi ,  Roland A. Cherwek ,  Paul C. Hamilton ,  David N. Martin

发明人： Gajanan H. Joshi ,  Roland A. Cherwek ,  Paul C. Hamilton ,  David N. Martin

IPC分类号： G01S736

CPC分类号： G01S7/021 ,  F41G7/301 ,  G01S5/02 ,  G01S13/003

摘要： (U) A system for protecting a strategic bomber approaching the field covered by an airborne surveillance radar is shown to include: A search receiver arrangement to detect interrogating pulses from such radar before detection by such radar is possible and to determine the range of such radar and an air-to-air guided missile adapted first to home on the source of the interrogating pulses and then to be guided to intercept by an active radar seeker.

摘要翻译： （U）用于保护接近机载监视雷达所覆盖的领域的战略轰炸机的系统被示为包括：用于在由这种雷达检测之前检测来自这种雷达的询问脉冲的搜索接收器装置是可能的并且确定这种雷达的范围 以及空对空导弹首先适应询问脉冲的来源，然后由主动雷达探测器引导拦截。

公开(公告)号：US5232182A

公开(公告)日：1993-08-03

申请号：US440390

申请日：1982-10-27

申请人： Paul C. Hamilton

发明人： Paul C. Hamilton

IPC分类号： F41G7/22 ,  F41G7/28

CPC分类号： F41G7/2206 ,  F41G7/2246 ,  F41G7/2286 ,  F41G7/28

摘要： A method of guiding an air-to-air missile launched from a penetrating aircraft at a target aircraft having a search radar therein is shown. The missile changes from a passive antiradiation homing mode to an active seeker mode when the missile is detected and the search radar is shutdown. The active seeker uses a synthetic aperture radar that is squinted at the target aircraft. At the handover point when the search radar is shutdown, the missile executes a turn away from the target aircraft to bring the target aircraft within the synthetic aperture radar coverage. The amount of turn is within preselected limits based on several parameters.

摘要翻译： 示出了在其中具有搜索雷达的目标飞机上从穿透飞机发射的空对空导弹的引导方法。 当检测到导弹并搜索雷达关闭时，导弹从被动反辐射归位模式转变为主动寻线器模式。 主动寻求者使用在目标飞机上眯眼的合成孔径雷达。 在搜索雷达停机的切换点，导弹执行远离目标飞机的转弯，将目标飞机带入合成孔径雷达覆盖范围。 根据几个参数，转弯量在预先选定的极限内。