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公开(公告)号:US09541763B1
公开(公告)日:2017-01-10
申请号:US14812508
申请日:2015-07-29
CPC分类号: G02B27/0179 , G01C23/00 , G02B27/01 , G02B2027/014
摘要: An active HUD boresight alignment system for correcting a boresight of a HUD in an aircraft relative to an aircraft boresight is described. The system has an aircraft IRU, a HUD angular orientation detector and a detector. The aircraft IRU is rigidly coupled with the aircraft and configured to define an aircraft boresight indicative of a three axis angular orientation of the aircraft. The HUD angular orientation detector is rigidly arranged relative to at least one component of the HUD in the aircraft, and configured to determine a HUD boresight indicative of a three axis angular orientation of the HUD. The processor is coupled with the aircraft IRU and the HUD angular orientation detector and configured to determine a boresight angular offset of the HUD boresight to the aircraft boresight for at least one axis of the three axis angular orientation, and to correct for the boresight angular offset based on the determined boresight angular offset.
摘要翻译: 描述了一种用于校正飞行器中相对于飞机视轴的HUD的视轴的主动HUD视轴对准系统。 该系统具有飞机IRU,HUD角度定向检测器和检测器。 飞机IRU与飞行器刚性联接并且被配置为限定指示飞机的三轴角度定向的飞行器视轴。 HUD角度方向检测器相对于飞行器中的HUD的至少一个部件刚性地布置,并且被配置为确定指示HUD的三轴角度取向的HUD视轴。 处理器与飞行器IRU和HUD角度定向检测器耦合,并且被配置成确定HUD视轴对于三轴角度取向的至少一个轴线的飞机视轴的视轴角度偏移,并且校正视轴角度偏移 基于确定的视轴角度偏移。