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Design and Flight Test of a Primary Flight Display Combined Vision System

机译:主飞行显示组合视觉系统的设计和飞行测试

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A series of flight tests were conducted to design and evaluate a Combined Vision System (CVS) that integrates a forward looking infrared video image with synthetic vision on a primary flight display. System features included colorizing the video image to mesh with the synthetic terrain background, decluttering the approach symbology to facilitate the detection of the approach lights and runway markings, creating a semi-transparent IR sky to ensure continuous situational awareness of the surrounding terrain, and annunciating the decision height to facilitate the transition to the actual runway environment. Over 100 approaches were flown during three flight test sessions. For the first flight test session pilots reviewed early CVS proofs of concept on Honeywell's Citation Sovereign. During the approach in low visibility conditions, the Pilot Flying remained head-down to 100 ft AGL, at which time he lifted his head and made a subjective judgment of whether he could easily and safely complete the transition to land before making a go-around. In the second flight test session enhancements included IR image coloring, IRS/GPS navigation system integration, and display annunciations. The series of flight tests culminated in a CVS integration on Honeywell's Gulfstream G450 aircraft for a direct head-up display (HUD) versus head-down display (HDD) comparison of the IR imagery. The HUD location is currently the standard for low visibility approaches with IR imagery. The G450 evaluation had three highly experienced pilots with an average of over 12,000 flight hours and over 2,500 hours with a HUD. They flew a total of 46 approaches, most to full-stop landings and many were in high workload conditions - low visibility weather or strong crosswinds. Again the Pilot Flying stayed head-down to 100 ft AGL and then transitioned to the outside view of actual runway environment before landing. Pilot performance with the CVS was equivalent to performance with the HUD on all flight parameters including glide-slope deviation, airspeed deviation, configuration to land at the crossing threshold, and the landing footprint on the runway. Workload scores and display ratings were equivalent between the two displays, giving a strong indication that the Honeywell CVS provides equivalent performance and an alternative means to the HUD for displaying the IR imagery.
机译:进行了一系列飞行测试,以设计和评估组合视觉系统(CVS),该系统在主飞行显示器上将前视红外视频图像与合成视觉集成在一起。系统功能包括将视频图像着色以与合成地形背景相啮合,对进场符号进行整理以促进对进场灯和跑道标记的检测,创建半透明的IR天空以确保对周围地形的连续情境感知并发出决定高度,以帮助过渡到实际跑道环境。在三个飞行测试阶段中,有100多个进场。在第一次飞行测试中,飞行员们回顾了霍尼韦尔(Choneywell)的《 Citation Sovereign》(Cover Sovereign)的早期CVS概念证明。在低能见度条件下的进近过程中,飞行员飞行头向下俯冲至100英尺AGL,这时他抬起头并做出主观判断,以确定他是否可以轻松安全地完成复飞之前的着陆。在第二次飞行测试中,增强功能包括IR图像着色,IRS / GPS导航系统集成和显示通知。该系列飞行测试最终完成了霍尼韦尔(Choosewell)湾流G450飞机上的CVS集成,从而可以对红外图像进行直接抬头显示(HUD)与抬头显示(HDD)的比较。 HUD位置当前是使用红外图像进行低能见度方法的标准。 G450评估由三名经验丰富的飞行员组成,他们的HUD平均飞行时间超过12,000小时,飞行时间超过2500小时。他们总共飞行了46个进近点,其中大多数都采取了全站着陆的方式,其中许多处于高工作量条件下-低能见度天气或强风。再次,飞行员飞行降落到100英尺AGL,然后在着陆之前过渡到实际跑道环境的外部视图。 CVS的飞行员性能等同于HUD在所有飞行参数上的性能,包括滑坡-斜度偏差,空速偏差,在交叉口起降的配置以及跑道的着陆足迹。两台显示器之间的工作负荷分数和显示器等级是相同的,这充分表明霍尼韦尔CVS可以提供​​同等的性能,并且是HUD用来显示红外图像的替代方法。

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