首页> 外国专利> HELICOPTER INTEGRATED FIRE AND FLIGHT CONTROL HAVING COORDINATED AREA BOMBING CONTROL

HELICOPTER INTEGRATED FIRE AND FLIGHT CONTROL HAVING COORDINATED AREA BOMBING CONTROL

机译:直升机集成的火灾和飞行控制具有协调的区域爆炸控制

摘要

During operation of a flight control system in a coordinated area bombing mode, one pair in a group of pairs of fire control azimuth coordinate error signal and elevation coordinate error signals are faded-in as the aircraft yaw attitude reference and pitch attitude reference, respectively. Each pair is respectively indicative of the change in aircraft yaw attitude and pitch attitude for an aircraft reference axis to be aligned with an aiming line of sight. The aiming line of sight corresponds to a target location within a selected target area. A firing signal is provided in response to both the azimuth and elevation coordinate error signals being below respective threshold magnitudes, and the next pair in the group of pairs of azimuth and elevation coordinate error signals provide the aircraft attitude reference. A selected weapon is fired in response to the firing signal.
机译:在协调区域轰炸模式下的飞行控制系统运行期间,成对的火控方位角坐标误差信号和仰角坐标误差信号对中的一对分别作为飞机的偏航姿态参考和俯仰姿态参考被淡入。每对分别指示要与瞄准瞄准线对准的飞机参考轴的飞机偏航姿态和俯仰姿态的变化。瞄准线对应于所选目标区域内的目标位置。响应于方位角和仰角坐标误差信号均低于各自的阈值幅度而提供了发射信号,并且方位角和仰角坐标误差对对的组中的下一对提供了飞机姿态参考。响应于发射信号发射选定的武器。

著录项

  • 公开/公告号EP0667005B1

    专利类型

  • 公开/公告日1997-01-15

    原文格式PDF

  • 申请/专利权人 UNITED TECHNOLOGIES CORPORATION;

    申请/专利号EP19930924913

  • 发明设计人 FOWLER DONALD W.;LAPPOS NICHOLOS D.;

    申请日1993-10-05

  • 分类号G05D1/08;F41G9/00;B64C13/50;

  • 国家 EP

  • 入库时间 2022-08-22 03:20:28

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