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1. 发明授权

EP3210091B1 OPTIMAL SAFE LANDING AREA DETERMINATION 有权
公开(公告)号：EP3210091B1
公开(公告)日：2020-02-19
申请号：EP15875863.1
申请日：2015-10-16
申请人： Sikorsky Aircraft Corporation
发明人： DING, Xuchu , DERENICK, Jason C. , ENGLOT, Brendan J. , CHEREPINSKY, Igor , SANE, Harshad S. , STATHIS, Christopher
IPC分类号： G05D1/00 , B64C39/02 , G05D1/06

2. 发明公开

EP3271743A1 TRAJECTORY CONTROL OF A VEHICLE 审中-公开
标题翻译：车辆的轨道控制
公开(公告)号：EP3271743A1
公开(公告)日：2018-01-24
申请号：EP16765465.6
申请日：2016-03-10
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , SANE, Harshad S.
IPC分类号： G01S13/94 , C05D1/00
CPC分类号： G05D1/102 , B64C13/16 , B64C39/024 , B64C2201/108 , B64C2201/141 , G01S13/94 , G05D1/101 , G08G5/0021 , G08G5/0039 , G08G5/0052 , G08G5/0086 , G08G5/045
摘要： A method of trajectory control for a vehicle includes obtaining an initial trajectory; presenting the initial trajectory as a current trajectory on an I/O device, the current trajectory presented overlaying terrain; initiating travel of the vehicle along the current trajectory; updating the current trajectory and the terrain in real time as the vehicle travels along the current trajectory; determining if change in the current trajectory is required; changing the current trajectory to an altered trajectory in response to determining change in the current trajectory is required; and presenting the altered trajectory on the I/O device, the altered trajectory presented overlaying the terrain.

3. 发明公开

EP3210091A2 OPTIMAL SAFE LANDING AREA DETERMINATION 有权
标题翻译：最佳安全着陆面积确定
公开(公告)号：EP3210091A2
公开(公告)日：2017-08-30
申请号：EP15875863.1
申请日：2015-10-16
申请人： Sikorsky Aircraft Corporation
发明人： DING, Xuchu , DERENICK, Jason C. , ENGLOT, Brendan J. , CHEREPINSKY, Igor , SANE, Harshad S. , STATHIS, Christopher
IPC分类号： G05D1/00
摘要： According to an aspect of the invention, a method of optimal safe landing area determination for an aircraft includes accessing a probabilistic safe landing area map that includes a plurality of probabilistic indicators of safe landing areas for the aircraft. A processing subsystem that includes one or more processing resources generates a list of candidate safe landing areas based on the probabilistic safe landing area map and one or more constraints. At least two of the candidate safe landing areas are provided to a path planner. The list of candidate safe landing areas is ranked based on results from the path planner indicating an estimated cost to reach each of the candidate safe landing areas. Based on the ranking, an indicator of an optimal safe landing area is output as a desired landing location for the aircraft.
摘要翻译：根据本发明的一个方面，一种用于飞机的最佳安全着陆区域确定方法包括：访问包括飞机安全着陆区域的多个概率指标的概率安全着陆区域地图。包括一个或多个处理资源的处理子系统基于概率安全着陆区域图和一个或多个约束来生成候选安全着陆区的列表。至少有两个候选安全着陆区被提供给路径规划者。候选安全着陆区域的列表根据路径规划者的结果进行排列，指示到达每个候选安全着陆区域的估计成本。基于排名，最优安全着陆区域的指标被输出为飞机的期望着陆位置。

4. 发明公开

EP3207336A1 SYNTHETIC VISION AUGMENTED WITH MULTISPECTRAL SENSING 审中-公开
标题翻译：用多光谱感应增强合成视觉
公开(公告)号：EP3207336A1
公开(公告)日：2017-08-23
申请号：EP15851355.6
申请日：2015-10-13
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , DERENICK, Jason C. , STATHIS, Christopher
IPC分类号： G01C23/00
CPC分类号： G01C23/005 , G01C23/00 , G06T1/60 , G06T15/005 , G06T15/04 , G06T17/20 , G09G5/36
摘要： A method for augmenting a synthetic vision system of a vehicle includes receiving, with a processor, signals indicative of real-time sensor data of a terrain for the vehicle via one or more acquisition devices; creating, with the processor, a terrain mesh of the terrain in response to the receiving of the sensor data; correlating, with the processor, the terrain mesh with preloaded terrain data of the terrain; creating, with the processor, a multispectral image of the terrain in response to the correlating the terrain mesh with the preloaded data; and texturing, with the processor, the terrain mesh for display on a display device.
摘要翻译：一种用于增强车辆的合成视觉系统的方法包括：利用处理器经由一个或多个获取设备接收指示车辆的地形的实时传感器数据的信号; 响应于接收到传感器数据，利用处理器创建地形的地形网格; 用处理器将地形网格与地形的预加载的地形数据相关联; 响应于将地形网格与预先加载的数据相关联，利用处理器创建地形的多光谱图像; 并利用处理器对地形网格进行纹理化以在显示设备上显示。

5. 发明授权

EP3198349B1 HAPTIC FEEDBACK FOR REALTIME TRAJECTORY CONSTRAINTS 有权
公开(公告)号：EP3198349B1
公开(公告)日：2019-11-06
申请号：EP15843757.4
申请日：2015-09-15
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , SANE, Harshad S.
IPC分类号： B64C13/10 , B64C27/57 , B64C13/00 , G05D1/10 , G06F3/0484 , G08G5/00

6. 发明公开

EP3218806A1 CENTRALIZED PROCESSING FOR AIRCRAFT OPERATIONS 审中-公开
标题翻译：航空器运行的集中处理
公开(公告)号：EP3218806A1
公开(公告)日：2017-09-20
申请号：EP15859282.4
申请日：2015-11-12
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , DELLARIPA, Daniel , THORNBERG, Christopher A. , HOWLAND, Gary
IPC分类号： G06F9/46
CPC分类号： G06F9/4881 , B64C27/06 , G05B15/02 , G06F9/4887 , G06F9/5083 , Y02D10/24
摘要： A system for centralizing computing operations for an aircraft, including a plurality of aircraft subsystems associated with the aircraft, a plurality of aircraft sensors associated with the aircraft, and a centralized processor to process the computing operations requested by each of the plurality of aircraft subsystems.
摘要翻译：一种用于集中包括与飞机相关联的多个飞机子系统的飞机的计算操作的系统，与飞机相关联的多个飞机传感器和集中处理器以处理由多个飞机子系统中的每一个请求的计算操作。

7. 发明公开

EP3198349A1 HAPTIC FEEDBACK FOR REALTIME TRAJECTORY CONSTRAINTS 有权
标题翻译：实时轨迹约束的HAPTIC反馈
公开(公告)号：EP3198349A1
公开(公告)日：2017-08-02
申请号：EP15843757.4
申请日：2015-09-15
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , SANE, Harshad S.
IPC分类号： G05D1/00
摘要： A system for receiving feedback in a flight plan of a vehicle includes a haptic-enabled device comprising a crew seat with an inceptor mounted thereto; and a processor with memory having instructions stored thereon that, when executed by the processor, cause the system to: receive signals indicative of the flight plan for the vehicle; receive deviation signals indicative of a proposed deviation in a trajectory for the flight plan; and transmit signals to the haptic-enabled device representing trajectory constraints in the proposed deviation in response to the receiving of the deviation signals.
摘要翻译：一种用于在车辆的飞行计划中接收反馈的系统包括：触觉使能设备，其包括安装有感应器的乘员座椅; 以及具有存储器的处理器，所述存储器上存储有指令，所述指令在由所述处理器执行时使得所述系统：接收指示所述车辆的所述飞行计划的信号; 接收指示所述飞行计划的轨迹中的建议偏差的偏差信号; 并且响应于偏差信号的接收而将信号发送到代表所提议偏差中的轨迹约束的启用触觉的设备。

8. 发明公开

EP2134598A2 VERTICAL SPEED AND FLIGHT PATH COMMAND ALGORITHM FOR DISPLACEMENT COLLECTIVE UTILIZING TACTILE CUEING AND TACTILE FEEDBACK 有权
标题翻译：垂直速度和route命令算法触觉高度控制和信令触觉反馈
公开(公告)号：EP2134598A2
公开(公告)日：2009-12-23
申请号：EP08795806.2
申请日：2008-03-18
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , SKAGGS, Michael R.
IPC分类号： B64C13/16 , B64C13/00
CPC分类号： G05D1/0858 , B64C13/503 , B64C27/04 , G05D1/0607
摘要： A flight control system includes a collective position command algorithm for a lift axis (collective pitch) which, in combination with an active collective system, provides a force feedback such that a pilot may seamlessly command vertical speed, flight path angle or directly change collective blade pitch. The collective position command algorithm utilizes displacement of the collective controller to command direct collective blade pitch change, while a constant force application to the collective controller within a 'level flight' detent commands vertical velocity or flight path angle. The 'level flight' detent provides a tactile cue for collective position to reference the aircraft level flight attitude without the pilot having to refer to the instruments and without excessive collective controller movement.

9. 发明授权

EP3171133B1 KINEMATIC MOTION PLANNING WITH REGIONAL PLANNING CONSTRAINTS 有权
公开(公告)号：EP3171133B1
公开(公告)日：2020-03-11
申请号：EP16199114.6
申请日：2016-11-16
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , DING, Xuchu , SANE, Harshad S.
IPC分类号： G01C21/20 , G08G5/00

10. 发明授权

EP2134598B1 VERTICAL SPEED AND FLIGHT PATH COMMAND ALGORITHM FOR DISPLACEMENT COLLECTIVE UTILIZING TACTILE CUEING AND TACTILE FEEDBACK 有权
公开(公告)号：EP2134598B1
公开(公告)日：2018-06-06
申请号：EP08795806.2
申请日：2008-03-18
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , SKAGGS, Michael R.
IPC分类号： B64C13/16 , B64C13/00 , G05D1/00 , G05D1/06
CPC分类号： G05D1/0858 , B64C13/503 , B64C27/04 , G05D1/0607
摘要： A flight control system includes a collective position command module for a lift axis (collective pitch) which, in combination with an active collective system, provides a force feedback such that a pilot may seamlessly command vertical speed, flight path angle or directly change collective blade pitch. The collective position command module utilizes displacement of the collective controller to command direct collective blade pitch change, while a constant force application to the collective controller within a “level flight” detent commands vertical velocity or flight path angle. The “level flight” detent provides a tactile cue for collective position to reference the aircraft level flight attitude without the pilot having to refer to the instruments and without excessive collective controller movement.

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