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2.发明授权FLY-BY-WIRE FLIGHT CONTROL SYSTEM WITH ELECTRONIC LEAD/LAG DAMPER ALGORITHM 有权FLY-BY-WIRE-FLUGSTEUERUNGSSYSTEM MIT ELEKTRONISCHEM LEAD / LAG-DÄMPFER-ALGORITHMUS
公开(公告)号：EP2170700B2
公开(公告)日：2017-05-03
申请号：EP08829369
申请日：2008-06-19
CPC分类号： B64C13/503 , G05D1/0858
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3.发明公开FLY-BY-WIRE FLIGHT CONTROL SYSTEM WITH ELECTRONIC LEAD/LAG DAMPER ALGORITHM 有权随着电子LEAD / LAG阻尼器算法FLY-BY-WIRE飞行控制系统
公开(公告)号：EP2170700A4
公开(公告)日：2013-04-24
申请号：EP08829369
申请日：2008-06-19
CPC分类号： B64C13/503 , G05D1/0858
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4.发明公开INTEGRATED HOVER DISPLAY WITH AUGMENTED APPROACH TO HOVER SYMBOLOGY CUEING FOR DEGRADED VISUAL ENVIRONMENTAL CONDITIONS 有权集成浮动显示与先进的方法对SYMBOLIC注浮动为贫困视力状况AROUND
公开(公告)号：EP1882157A4
公开(公告)日：2012-08-01
申请号：EP06784368
申请日：2006-04-20
CPC分类号： H04L29/06 , G01C23/00 , G05D1/102 , G08G5/0095 , H04L67/125 , H04L69/329
摘要： A flight control system includes a primary flight display having a hover display which facilitates operations in DVE conditions. The hover display includes a radar altitude display, heading drift symbology and lateral drift symbology which assists pilots in the detection of drift, which is common in DVE situations and to provide the pilot with a salient cue pertinent to the approach to hover and landing.
摘要翻译： 的飞行控制系统包括具有显示悬停其中在DVE条件便于操作的主飞行显示。 悬停显示器包括雷达高度显示，航向漂移符号和横向漂移符号，这有助于导频在检测漂移，所有这些是在DVE情况常见并提供一种具有显着的提示相关的悬停在进场和着陆的导频。
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公开(公告)号：EP2976260A4
公开(公告)日：2016-10-19
申请号：EP14807547
申请日：2014-03-12
IPC分类号： B64C27/635 , B64C27/57 , B64C27/605
CPC分类号： B64C27/57 , B64C27/605 , B64C27/635
摘要： A control system for a rotor assembly includes a plurality of sensors configured to detect a lead-lag rate of each rotor blade of a plurality of rotor blades rotatable around a shaft and a flight control computer configured to generate lead-lag compensation signals based on the detected lead rate and lag rate of each rotor blade to control each rotor blade.
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6.发明公开ROTARY WING AIRCRAFT FLIGHT CONTROL SYSTEM WITH A PROXIMITY CUEING AND AVOIDANCE SYSTEM 审中-公开控制系统与PROXIMITÄTSSIGNAL和回避系统中的摇摆机
公开(公告)号：EP1917498A4
公开(公告)日：2014-01-01
申请号：EP06801777
申请日：2006-08-17
CPC分类号： G05D1/0858 , G01S13/9303 , G01S17/933 , G08G5/0021 , G08G5/045
摘要： A method of obstacle avoidance for a rotary wing aircraft includes detecting an obstacle proximate to the aircraft and commanding a servo to generate a force to an input control device in a direction that tends to preclude the aircraft from contacting the detected obstacle, the command having lesser authority than a pilot input command.
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7.发明公开MODEL BASED SENSOR SYSTEM FOR LOADS AWARE CONTROL LAWS 审中-公开MODEMBASIERTES SENSORSYSTEMFÜRLASTENBEWUSSTE STEUERUNGSREGELN
公开(公告)号：EP2168022A4
公开(公告)日：2013-06-05
申请号：EP08827787
申请日：2008-05-30
发明人： SAHASRABUDHE VINEET , FAYNBERG ALEX
CPC分类号： B64C27/57 , G05D1/0858
摘要： A flight control system includes a model-based sensor system which estimates angular accelerations to control rotor system moment such that loads on the aircraft structure are reduced to thereby allow an aircraft structural envelope to more closely follow an aircraft service flight envelope.
摘要翻译： 飞行控制系统包括基于模型的传感器系统，其估计角加速度以控制转子系统时刻，使得飞行器结构上的载荷减小，从而允许飞行器结构信封更紧密地遵循飞机服务飞行信封。
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">8.发明公开TECHNICAL DESIGN CONCEPTS TO IMPROVE HELICOPTER OBSTACLE AVOIDANCE AND OPERATIONS IN "BROWNOUT" CONDITIONS 审中-公开技术的设计理念，完善条款掉电操作的直升机与避障
公开(公告)号：EP1616228A4
公开(公告)日：2013-05-29
申请号：EP04775864
申请日：2004-03-31
CPC分类号： H04L67/125 , G01C23/00 , G05D1/102 , H04L29/06 , H04L69/329
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