公开(公告)号：WO1994010616A1

公开(公告)日：1994-05-11

申请号：PCT/US1993009500

申请日：1993-10-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  FOWLER, Donald, W. ,  LAPPOS, Nicholos, D.

IPC: G05D01/08

CPC classification number: B64C13/503 ,  F41G3/22 ,  F41G5/18 ,  F41G9/002 ,  G05D1/0858

Abstract: 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 (145) 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 (685) 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.

Abstract translation: 在协调区域轰炸模式下的飞行控制系统的操作期间，一组火控方位坐标误差信号和仰角坐标误差信号（145）中的一对作为飞机偏航姿态参考和俯仰姿态参考 ， 分别。 每一对分别表示与瞄准视线对准的飞行器参考轴的飞行器偏航姿态和俯仰姿态的变化。 目标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两者都低于相应的阈值幅度而提供点火信号（685），并且该组方位角和仰角坐标误差信号组中的下一对提供飞机姿态参考。 选择的武器是响应发射信号而被触发的。

公开(公告)号：EP0667005B1

公开(公告)日：1997-01-15

申请号：EP93924913.2

申请日：1993-10-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： FOWLER, Donald, W. ,  LAPPOS, Nicholos, D.

IPC: G05D1/08 ,  F41G9/00 ,  B64C13/50

CPC classification number: B64C13/503 ,  F41G3/22 ,  F41G5/18 ,  F41G9/002 ,  G05D1/0858

Abstract: 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 (145) 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 (685) 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.

公开(公告)号：EP0667005A1

公开(公告)日：1995-08-16

申请号：EP93924913.0

申请日：1993-10-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： FOWLER, Donald, W. ,  LAPPOS, Nicholos, D.

IPC: B64C13 ,  F41G3 ,  F41G5 ,  F41G9 ,  G05D1

CPC classification number: B64C13/503 ,  F41G3/22 ,  F41G5/18 ,  F41G9/002 ,  G05D1/0858

Abstract: 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 (145) 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 (685) 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.