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1. 发明授权

EP0667005B1 HELICOPTER INTEGRATED FIRE AND FLIGHT CONTROL HAVING COORDINATED AREA BOMBING CONTROL 失效
标题翻译：综合飞行控制，并用火炸弹袭击CONTROL协调
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
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： FOWLER, Donald, W. , LAPPOS, Nicholos, D.
IPC分类号： G05D1/08 , F41G9/00 , B64C13/50
CPC分类号： B64C13/503 , F41G3/22 , F41G5/18 , F41G9/002 , G05D1/0858
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 (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.

2. 发明公开

EP0226026A2 Aircraft automatic boresight correction 失效
标题翻译：飞机自动视轴校正
公开(公告)号：EP0226026A2
公开(公告)日：1987-06-24
申请号：EP86115391.4
申请日：1986-11-06
申请人： GENERAL ELECTRIC COMPANY
发明人： Hickin, Charles Wyndham Robinson , Tye, Gene
IPC分类号： F41G3/22 , F41G5/18
CPC分类号： F41G3/323 , F41G3/142 , F41G3/22 , F41G5/18
摘要： A boresight correction system is disclosed that determines the existing error between an aircraft gunsight and its gun systems while prescribed aircraft maneuvers are performed and which automaticaily corrects the gunsight system to compensate for this error. The system includes a sensor for detecting bullet positions, hardware that determines the bullet positions relative to the gun boresight, a digital processor to determine the above mentioned error, and to correct the gunsight system according to this error, and a non-volatile memory in the digital processor to store a corrected boresight position.
摘要翻译：公开了一种视轴校正系统，该系统确定在执行规定的飞机操纵时飞机瞄准器与其枪系统之间的现有误差，并自动校正瞄准系统以补偿该误差。该系统包括用于检测子弹位置的传感器，用于确定相对于枪瞄的子弹位置的硬件，用于确定上述错误的数字处理器，以及根据该错误修正枪瞄系统，以及非易失性存储器数字处理器存储纠正的视轴位置。

3. 发明公开

EP0077273A1 Système de conduite de tir pour une arme à tir tendu montée sur un aéronef à voilure tournante 失效
标题翻译：安装有旋转翼飞行器上用于与平射轨道武器火力控制。
公开(公告)号：EP0077273A1
公开(公告)日：1983-04-20
申请号：EP82401872.5
申请日：1982-10-12
申请人： AEROSPATIALE Société Nationale Industrielle
发明人： Brunello, Alain Michel , Catani, Guy Gabriel
IPC分类号： F41G5/18
CPC分类号： F41G5/18
摘要： Système de conduite de tir pour une arme à tir tendu (1) montée sur un aéronef à voilure tournante, susceptible d'être acionné par le pilote lui-même et comportant une calculatrice électronique, ladite arme (1) étant montée rotative autour de deux axes Y-Y' et Z-Z' transversaux grâce à des moyens moteurs commandés par ladite calculatrice.
Selon l'invention, ce système de conduite de tir est caractérisé en ce qu'il comporte un système de visée (4) sur lequel sont susceptibles d'apparaître simultanément une cible (6) et un repère (8'), ledit repère pouvant être déplacé sur ledit système de visée par une commande du pilote, ainsi que des moyens (7) pour déterminer les coordonnées de la position dudit repère (8) et les transmettre à ladite calculatrice électronique (13) au moins lorsque sur ledit système de visée (4) ledit repère (8') est amené en superposition à ladite cible (6).

4. 发明公开

EP4414654A1 METHODS AND APPARATUS FOR POINTING LOGIC IN AIRCRAFT 审中-公开
公开(公告)号：EP4414654A1
公开(公告)日：2024-08-14
申请号：EP24153632.5
申请日：2024-01-24
申请人： The Boeing Company
发明人： FAMULARO, Douglas , SAUNDERS, Jeffery
IPC分类号： F41G3/14 , F41G3/22 , F41G5/16 , F41G5/18 , F41G9/00 , B64U101/18 , F41G5/22
CPC分类号： B64U2101/1820230101 , F41G3/22 , F41G5/18 , F41G9/002 , B64D7/06 , B64U10/14
摘要： Methods and apparatus for pointing logic in aircraft are disclosed. A disclosed example apparatus to aim an aiming device carried by an aircraft includes at least one memory, machine readable instructions, and processor circuitry. The processor is to at least one of instantiate or execute the machine readable instructions to determine a position of a target, determine an orientation of the aircraft, determine aiming points based on the orientation and a movement range of the aiming device, and determine a movement of at least one of the aircraft or the aiming device based on the aiming points and the position to orient the aiming device toward the target.

5. 发明公开

EP0226026A3 Aircraft automatic boresight correction 失效
标题翻译：飞机自动BORESIGHT校正
公开(公告)号：EP0226026A3
公开(公告)日：1990-04-04
申请号：EP86115391.4
申请日：1986-11-06
申请人： GENERAL ELECTRIC COMPANY
发明人： Hickin, Charles Wyndham Robinson , Tye, Gene
IPC分类号： F41G3/22 , F41G5/18
CPC分类号： F41G3/323 , F41G3/142 , F41G3/22 , F41G5/18
摘要： A boresight correction system is disclosed that determines the existing error between an aircraft gunsight and its gun systems while prescribed aircraft maneuvers are performed and which automaticaily corrects the gunsight system to compensate for this error. The system includes a sensor for detecting bullet positions, hardware that determines the bullet positions relative to the gun boresight, a digital processor to determine the above mentioned error, and to correct the gunsight system according to this error, and a non-volatile memory in the digital processor to store a corrected boresight position.

6. 发明授权

EP0093603B1 Moving target ordnance control 失效
标题翻译：移动目标监控
公开(公告)号：EP0093603B1
公开(公告)日：1989-01-04
申请号：EP83302455.7
申请日：1983-04-29
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： Boles, Sol , Smrek, Walter J.
IPC分类号： G01S13/52
CPC分类号： G01S13/52 , F41G5/18 , F41G9/002 , G01S13/9029

7. 发明公开

EP0105432A2 Aircraft automatic boresight correction 失效
标题翻译： Automaticallyche SchussverbesserungfürFlugzeuge。
公开(公告)号：EP0105432A2
公开(公告)日：1984-04-18
申请号：EP83109535.1
申请日：1983-09-24
申请人： GENERAL ELECTRIC COMPANY
发明人： Hickin, Charles Wyndham Robinson , Tye, Gene
IPC分类号： F41G5/18 , F41G3/14
CPC分类号： F41G5/18 , F41G3/142 , F41G3/323
摘要： A system that determines the error existing between the aircraft gunsight and the gun systems, while prescribed aircraft maneuvres are performed, and automatically corrects the gunsight system to compensate for this error. The system includes a bullet sensor, such as a television camera, hardware that determines the bullet positions relative to the gun boresight, computational means to determine the above mentioned error, and means to store the error and correct the gunsight system according to this error. This system yields a lower cost, more accurate, and more convenient method requiring less skilled labor than that presently used to accomplish the same result.
摘要翻译：确定飞机瞄准枪和枪系统之间存在的错误的系统，同时执行规定的飞机操作，并自动更正瞄准系统以补偿此错误。该系统包括诸如电视摄像机的子弹传感器，确定相对于枪视线的子弹位置的硬件，用于确定上述错误的计算装置，以及根据该错误来存储错误并修正瞄准系统的装置。该系统产生比目前用于实现相同结果的较低成本，更准确和更方便的方法，其需要较少的熟练劳动力。

8. 发明公开

EP0093603A1 Moving target ordnance control 失效
标题翻译： Ziele的Feuerleiteinrichtungfürbewegliche。
公开(公告)号：EP0093603A1
公开(公告)日：1983-11-09
申请号：EP83302455.7
申请日：1983-04-29
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： Boles, Sol , Smrek, Walter J.
IPC分类号： G01S13/52
CPC分类号： G01S13/52 , F41G5/18 , F41G9/002 , G01S13/9029
摘要： in an airborne radar system, moving ground targets are. identified on a cathode ray tube (CRT) display and their motion tracked to allow precise delivery of air-to-ground weapons. Target location errors, due to the effect of target motion upon the doppler frequency of the received radar signals, are significantly reduced. The target's radial velocity with respect to the electrical boresight of the system antenna is determined and a corresponding frequency adjustment is made to the processed signal in order to locate the target accurately on the display so as to lie in precise correspondence with its displayed stationary surroundings.
The measurement of target radial velocity also provides a precise interferometer antenna referenced azimuth angle estimate to be used for relative range and azimuth weapon guidance, independent of usually large angle errors arising from clutter effects within the field of view of the antenna, and of other hardware and navigational error sources associated with absolute angle measurement systems.
摘要翻译：在机载雷达系统中，移动地面目标在阴极射线管（CRT）显示器上被识别，并且其运动被跟踪以允许精确地传送空对地武器。由于目标运动对所接收的雷达信号的多普勒频率的影响，目标定位误差显着降低。确定目标相对于系统天线的电视距的径向速度，并对处理的信号进行对应的频率调整，以便将目标准确地定位在显示器上，以便与其所显示的静止环境精确对应。目标径向速度的测量还提供了一种精确的干涉仪天线参考方位角估计，用于相对范围和方位武器指导，而与通常由天线视野内的杂波效应引起的大角度误差无关，而其他硬件和与绝对角度测量系统相关的导航误差源。

9. 发明公开

EP1561082A4 REAL TIME DYNAMICALLY CONTROLED ELEVATION AND AZIMUTH GUN POD MOUNTED ON A FIXED-WING AERIAL COMBAT VEHICLE 审中-公开
标题翻译：在STARR翼战斗机装式CANNON集装箱，动态仰角和方位角实时控制
公开(公告)号：EP1561082A4
公开(公告)日：2009-04-29
申请号：EP03720840
申请日：2003-05-15
申请人： PADAN NIR
发明人： PADAN NIR
IPC分类号： F41A27/02 , B64D7/06 , F41A27/06 , F41A27/28 , F41A27/30
CPC分类号： F41A27/02 , B64D7/06 , F41A27/06 , F41A27/28 , F41A27/30 , F41G5/18
摘要： A gun pod, mounted on a fixed-wing aerial vehicle, stores, delivers, controls and supports a controllable movement gun unit. The gun pod includes a flexible gun mount, gun movement actuators, gun movement controllers, a standalone range finder, a standalone processor, and standalone sensors for capturing dynamically environmental data and for controlling the movement of the gun unit. The gun is provided with allowable ranges of movement in the elevation and the azimuth where the ranges are determined in accordance with the flight envelope of the aerial vehicle, the characteristics of the gun unit and the mounting location of the gun pod. The movement of the gun is either controlled manually or automatically.

10. 发明授权

EP0736166B1 HELICOPTER INTEGRATED FIRE AND FLIGHT CONTROL HAVING A PRE-LAUNCH AND POST-LAUNCH MANEUVER DIRECTOR 失效
标题翻译：综合火力和飞行控制FOR之前，控制系统，直升机在发射后
公开(公告)号：EP0736166B1
公开(公告)日：1998-07-01
申请号：EP95904907.3
申请日：1994-12-02
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： FOWLER, Donald, W. , LAPPOS, Nicolas, D. , EDWARDS, Joan, A.
IPC分类号： F41G9/00 , F41G5/18 , G05D1/08
CPC分类号： F41G7/007 , F41G5/18 , F41G9/002 , G05D1/085

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