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1. 发明公开

EP2290491A2 Incremental position-based guidance for a UAV 审中-公开
标题翻译：以色列无人机
公开(公告)号：EP2290491A2
公开(公告)日：2011-03-02
申请号：EP10165748.4
申请日：2010-06-11
申请人： Honeywell International Inc.
发明人： Hamke, Eric , Trujillo, Matthew , Brown, Philip
IPC分类号： G05D1/10
CPC分类号： G05D1/101
摘要： Disclosed herein is a method and system for flying a ducted-fan aerial vehicle, such as an unmanned aerial vehicle (UAV). The method includes receiving a flight plan comprising a plurality of waypoints and a plurality of path segments connecting the plurality of waypoints in an order of execution. The method further includes determining actual flight instructions for the ducted fan unmanned aerial vehicle based on (i) the received flight plan, (ii) a predetermined set of operating parameters associated with the ducted fan unmanned aerial vehicle, and (iii) an iterative analysis of a plurality of ordered triples. The method further includes sending the actual flight instructions to at least one processor of the ducted fan unmanned aerial vehicle configured to implement one or more portions of the actual flight instructions.
摘要翻译：本文公开了一种用于飞行诸如无人驾驶飞行器（UAV）的风扇式飞行器的方法和系统。该方法包括接收包括多个航路点的飞行计划和以执行顺序连接多个航路点的多个路径段。该方法还包括基于（i）接收到的飞行计划，（ii）与管道风扇无人机相关联的预定的一组操作参数，以及（iii）迭代分析来确定管道风扇无人机的实际飞行指令的多个有序三元组。该方法还包括将实际飞行指令发送到配置成实现实际飞行指令的一个或多个部分的管道风扇无人机的至少一个处理器。

2. 发明公开

EP2594484A2 Unmanned air vehicle fault tolerant flight control system and method 审中-公开
标题翻译： Unbemanntes Luftfahrzeug mit fehlertolerantem Flugsteuerungssystem und -Verfahren
公开(公告)号：EP2594484A2
公开(公告)日：2013-05-22
申请号：EP12184149.8
申请日：2012-09-12
申请人： Honeywell International Inc.
发明人： Hamke, Eric Ehrhardt , Trujillo, Matthew , Enns, Dale
IPC分类号： B64C39/02 , G05D1/00
CPC分类号： B64C39/024 , B64C2201/108 , B64C2201/14 , G05D1/0055 , G05D1/0858
摘要： Methods and apparatus are provided for controlling an unmanned air vehicle (UAV) that includes a plurality of independently controllable control vanes. Control vane position commands are supplied that will move each of the control vanes to a position that will cause the UAV to implement a commanded maneuver. Inoperability of one of the control vanes is sensed, and the position of the inoperable control vane is determined. New control vane position commands are determined, based on the determined position of the inoperable control vane, which will also cause the UAV to implement the commanded maneuver.
摘要翻译：提供了用于控制包括多个可独立控制的控制叶片的无人驾驶飞行器（UAV）的方法和装置。提供控制叶片位置命令，其将每个控制叶片移动到将使UAV执行命令的操纵的位置。检测到其中一个控制叶片的不能操作，并确定不可操作的控制叶片的位置。基于不可操作的控制叶片的确定位置确定新的控制叶片位置命令，这也将使无人机实现命令的操纵。

3. 发明公开

EP2290491A3 Incremental position-based guidance for a UAV 审中-公开
标题翻译：用于UAV增量基于位置的引导
公开(公告)号：EP2290491A3
公开(公告)日：2012-09-05
申请号：EP10165748.4
申请日：2010-06-11
申请人： Honeywell International Inc.
发明人： Hamke, Eric , Trujillo, Matthew , Brown, Philip
IPC分类号： G05D1/10
CPC分类号： G05D1/101
摘要： Disclosed herein is a method and system for flying a ducted-fan aerial vehicle, such as an unmanned aerial vehicle (UAV). The method includes receiving a flight plan comprising a plurality of waypoints and a plurality of path segments connecting the plurality of waypoints in an order of execution. The method further includes determining actual flight instructions for the ducted fan unmanned aerial vehicle based on (i) the received flight plan, (ii) a predetermined set of operating parameters associated with the ducted fan unmanned aerial vehicle, and (iii) an iterative analysis of a plurality of ordered triples. The method further includes sending the actual flight instructions to at least one processor of the ducted fan unmanned aerial vehicle configured to implement one or more portions of the actual flight instructions.

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