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1. 发明申请

US20130311009A1 FLIGHT TECHNICAL CONTROL MANAGEMENT FOR AN UNMANNED AERIAL VEHICLE 失效
标题翻译：用于无人驾驶飞机的飞行技术控制管理
公开(公告)号：US20130311009A1
公开(公告)日：2013-11-21
申请号：US13932623
申请日：2013-07-01
申请人： Honeywell International Inc.
发明人： Katherine McAndrew , Linda J. Watson , Jon Feist , A. Christopher Moorman
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , G05D1/0038 , G05D1/0077 , G05D1/0088
摘要： Two architectures for unmanned aerial vehicles (UAVs) and a method for executing a mission plan are provided. One architecture for a UAV includes a flight command and mission execution (FCME) component making strategic decisions, a flight technical control manager (FTCM) making tactical decisions and a vehicle management system (VMS) providing navigational support. The FCME and FTCM execute on one processor and the VMS executes on a separate processor. The second architecture includes redundant processors for executing the FCME and FTCM as well as redundant processors for executing the VMS. The UAV executes a mission plan, which may include flight plan(s), communication plan(s), weapons plan(s), sensor plan(s), and/or contingent flight plan(s). The UAV may control various optical sensors, training sensors, and lights as well.
摘要翻译：提供了两种无人机（UAV）的架构和执行任务计划的方法。无人机的一个架构包括飞行命令和任务执行（FCME）组成战略决策，飞行技术控制经理（FTCM）进行战术决策和提供导航支持的车辆管理系统（VMS）。 FCME和FTCM在一个处理器上执行，VMS在单独的处理器上执行。第二种架构包括用于执行FCME和FTCM的冗余处理器以及用于执行VMS的冗余处理器。无人机执行任务计划，其中可能包括飞行计划，通信计划，武器计划，传感器计划和/或或有飞行计划。无人机还可以控制各种光学传感器，训练传感器和灯光。

2. 发明授权

US08600602B1 Flight technical control management for an unmanned aerial vehicle 失效
公开(公告)号：US08600602B1
公开(公告)日：2013-12-03
申请号：US13932623
申请日：2013-07-01
申请人： Honeywell International Inc.
发明人： Katherine McAndrew , Linda J. Watson , Jon Feist , A. Christopher Moorman
IPC分类号： G01C22/00 , B64C13/16 , G09B9/08
CPC分类号： B64C19/00 , G05D1/0038 , G05D1/0077 , G05D1/0088
摘要： Two architectures for unmanned aerial vehicles (UAVs) and a method for executing a mission plan are provided. One architecture for a UAV includes a flight command and mission execution (FCME) component making strategic decisions, a flight technical control manager (FTCM) making tactical decisions and a vehicle management system (VMS) providing navigational support. The FCME and FTCM execute on one processor and the VMS executes on a separate processor. The second architecture includes redundant processors for executing the FCME and FTCM as well as redundant processors for executing the VMS. The UAV executes a mission plan, which may include flight plan(s), communication plan(s), weapons plan(s), sensor plan(s), and/or contingent flight plan(s). The UAV may control various optical sensors, training sensors, and lights as well.

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