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61. 发明申请

US20170310749A1 METHODS AND APPARATUS FOR FLIGHT BRIEFING DATA SYNCHRONIZATION 审中-公开
公开(公告)号：US20170310749A1
公开(公告)日：2017-10-26
申请号：US15137546
申请日：2016-04-25
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Jiri Vasek , Petr Tieftrunk , Zdenek Eichler , Jan Bilek
IPC分类号： H04L29/08 , H04L29/06
CPC分类号： H04L67/1095 , G08G5/0013 , G08G5/0021 , G08G5/0034 , G08G5/0039 , G08G5/0091 , H04L65/1069 , H04L67/12
摘要： A method for managing a flight briefing data system is provided. The method establishes, by a central computer system, a first communication connection with an electronic device and a second communication connection with an aircraft onboard avionics unit; transmits, by the central computer system, flight briefing data via the first communication connection and the second communication connection, wherein the flight briefing data comprises at least a plurality of Notices to Airmen (NOTAMs) associated with a pending flight; receives, by the central computer system, altered flight briefing data; and synchronizes the central computer system, the electronic device, and the aircraft onboard avionics unit, by transmitting the altered flight briefing data via the first communication connection and the second communication connection.

62. 发明申请

US20170309191A1 SYSTEM AND METHOD FOR CONTROLLING AUTONOMOUS FLYING VEHICLE FLIGHT PATHS 审中-公开
公开(公告)号：US20170309191A1
公开(公告)日：2017-10-26
申请号：US15644723
申请日：2017-07-07
申请人： AirMap, Inc.
发明人： Benjamin Daniel MARCUS
IPC分类号： G08G5/00 , B64C39/02
CPC分类号： G08G5/0034 , B64C39/024 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/146 , G08G5/0008 , G08G5/0013 , G08G5/0039 , G08G5/006 , G08G5/0069 , G08G5/0078 , G08G5/0091
摘要： A method is provided for limiting access to airspace by drones. The method includes receiving position information from a user associated with a property identified by the position information. The method also includes assembling the position information with other position information to compile a comprehensive configurable flight zone database. The method further includes pushing the configurable flight zone database to at least one drone. The drone accesses the configurable flight zone database to determine if movement is allowed, and the drone is programmed to not fly into areas identified in the configurable flight zone database. In the method, the drone may be further programmed to prohibit directing a camera into the areas identified in the configurable flight zone database.

63. 发明申请

US20170302364A1 UNMANNED VEHICLE, SYSTEM AND METHOD FOR TRANSMITTING SIGNALS 审中-公开
公开(公告)号：US20170302364A1
公开(公告)日：2017-10-19
申请号：US15637978
申请日：2017-06-29
申请人： PROXY TECHNOLOGIES, INC.
发明人： Patrick C. CESARANO
IPC分类号： H04B7/185 , H01Q3/36 , G05D1/00 , H04B7/06 , H01Q3/28 , G01S13/06 , G01S13/02
CPC分类号： G05D1/0214 , B64C39/024 , B64C2201/021 , B64C2201/024 , B64C2201/141 , B64C2201/143 , B64C2201/146 , G01B9/021 , G01B11/00 , G01C21/165 , G01N21/8851 , G01N27/20 , G01N2201/12 , G01S7/006 , G01S13/02 , G01S13/06 , G01S13/42 , G01S15/02 , G01S19/13 , G01S2013/0254 , G05B11/42 , G05B13/024 , G05B13/042 , G05D1/0022 , G05D1/0027 , G05D1/0088 , G05D1/0094 , G05D1/02 , G05D1/0202 , G05D1/0204 , G05D1/0206 , G05D1/021 , G05D1/0246 , G05D1/0278 , G05D1/104 , G05D2201/0207 , G06K9/00637 , G06K9/00677 , G08G5/0039 , G08G5/045 , G08G9/02 , H01Q3/26 , H01Q3/2617 , H01Q3/28 , H01Q3/36 , H04B7/0617 , H04B7/18506 , H04N5/225 , H04N7/183 , H04N2005/2255
摘要： Some embodiments are directed to an unmanned vehicle for transmitting signals. The unmanned vehicle includes a transmitting unit that is configured to transmit a signal towards an object. The unmanned vehicle also includes a control unit that is in communication with at least one companion unmanned vehicle. The control unit is configured to determine a position of the at least one companion unmanned vehicle relative to the unmanned vehicle. The control unit is further configured to control the transmitting element based on at least the position of the at least one unmanned vehicle such that the transmitting element forms a phased-array transmitter with a transmitting element of the at least one companion unnamed vehicle, the phased-array transmitter emitting a transmission beam in a predetermined direction.

64. 发明申请

US20170263133A1 PROGRAMMING LANGUAGE FOR EXECUTION BY DRONE 审中-公开
公开(公告)号：US20170263133A1
公开(公告)日：2017-09-14
申请号：US15064542
申请日：2016-03-08
申请人： International Business Machines Corporation
发明人： Jeanette L. Blomberg , Eric K. Butler , Anca A. Chandra , Pawan R. Chowdhary , Thomas D. Griffin , Divyesh Jadav , Shun Jiang , Sunhwan Lee , Robert J. Moore , Hovey R. Strong, JR. , Chung-hao Tan
IPC分类号： G08G5/00 , G01W1/10 , B64C39/02
CPC分类号： G08G5/0039 , B64C39/024 , B64C2201/141 , G01W1/10 , G08G5/0004 , G08G5/0013 , G08G5/0021 , G08G5/0026 , G08G5/0056 , G08G5/0069 , G08G5/0091
摘要： One embodiment provides a method comprising maintaining a weather model based on predicted weather conditions for an air traffic control zone. A hash table comprising multiple hash entries is maintained. Each hash entry comprises a timestamped predicted weather condition for a cell in the zone. A flight plan request for a drone is received. The request comprises a planned flight path for the drone. For at least one cell on the planned flight path, same latitude or same longitude cells, whichever is most closely orthogonal to a direction of the planned flight path, are heuristically probed. Weather conditions for the at least one cell are estimated based on predicted weather conditions for the same latitude or same longitude cells. An executable flight plan is generated if the planned flight path is feasible based on the estimated weather conditions; otherwise, a report including an explanation of infeasibility is generated instead.

65. 发明申请

US20170263132A1 DRONE AIR TRAFFIC CONTROL AND FLIGHT PLAN MANAGEMENT 有权
公开(公告)号：US20170263132A1
公开(公告)日：2017-09-14
申请号：US15064536
申请日：2016-03-08
申请人： International Business Machines Corporation
发明人： Eric K. Butler , Anca A. Chandra , Pawan R. Chowdhary , Susanne M. Glissmann-Hochstein , Thomas D. Griffin , Divyesh Jadav , Sunhwan Lee , Hovey R. Strong, JR.
IPC分类号： G08G5/00
CPC分类号： G08G5/0039 , G08G5/0013 , G08G5/0026 , G08G5/0069 , G08G5/0082
摘要： One embodiment provides a method comprising receiving a flight plan request for a drone. The flight plan request comprises a drone identity, departure information, and arrival information. The method further comprises constructing a modified flight plan for the drone based on the flight plan request, wherein the modified flight plan represents an approved, congestion reducing, and executable flight plan for the drone, and the modified flight plan comprises a sequence of four-dimensional (4D) cells representing a planned flight path for the drone. For each 4D cell of the modified flight plan, the method further comprises attempting to place an exclusive lock on behalf of the drone on the 4D cell, and in response to a failure to place the exclusive lock on behalf of the drone on the 4D cell, rerouting the modified flight plan around the 4D cell to a random neighboring 4D cell.

66. 发明申请

US20170251181A1 Immersive Interactive Telepresence 审中-公开
公开(公告)号：US20170251181A1
公开(公告)日：2017-08-31
申请号：US15056983
申请日：2016-02-29
申请人： Microsoft Technology Licensing, LLC
发明人： Nikolai Smolyanskiy , Zhengyou Zhang , Vikram R. Dendi , Michael Hall
IPC分类号： H04N7/18 , B64C39/02 , G05D1/00 , G08G9/02 , H04L29/06
CPC分类号： H04N7/185 , B64C39/024 , B64C2201/127 , B64C2201/141 , B64C2201/146 , G01C21/3484 , G05D1/0016 , G05D1/0038 , G05D1/005 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/006 , G08G5/0069 , G08G5/0082 , H04L67/38
摘要： In embodiments of immersive interactive telepresence, a system includes a vehicle that captures an experience of an environment in which the vehicle travels, and the experience includes audio and video of the environment. User interactive devices receive the audio and the video of the environment, and each of the user interactive devices represent the experience for one or more users who are remote from the environment. A trajectory planner is implemented to route the vehicle based on obstacle avoidance and user travel intent as the vehicle travels in the environment. The trajectory planner can route the vehicle to achieve a location objective in the environment without explicit direction input from a vehicle operator or from the users of the user interactive devices.

67. 发明授权

US09747807B2 Systems and methods for displaying quick preview notices to airmen 有权
公开(公告)号：US09747807B2
公开(公告)日：2017-08-29
申请号：US14606337
申请日：2015-01-27
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Subash Samuthirapandian , Markus Alan Johnson , Pramod Kumar Malviya , Jayasenthilnathan B , Bretislav Passinger
IPC分类号： G06F19/00 , G06G7/70 , G06G7/76 , G08G5/00 , G08G5/06 , G01C23/00
CPC分类号： G08G5/0021 , G01C23/00 , G08G5/0013 , G08G5/003 , G08G5/0039 , G08G5/06
摘要： A flight display system or method in accordance with this disclosure involves the presentation, on an aircraft, of a “quick preview” notice to airmen (“NOTAM”) display that includes a plurality of stacked flight route portion boxes, each of the plurality of flight route portion boxes pertaining to and being labeled as one of: a departure taxiing portion, a standard instrument departure portion, an en route portion, a standard terminal arrival route portion, an approach portion, and an arrival taxiing portion; each of the plurality of flight route portion boxes graphically displaying flight route symbology pertaining to and labeled as each airport taxiing reference point and/or each aeronautical waypoint that falls within its labeled flight route portion; and wherein at least one of the plurality of flight route portion boxes further graphically displays NOTAM symbology pertaining to at least one of the NOTAMs that are relevant to the flight route.

68. 发明申请

US20170243496A1 DYNAMIC TURBULENCE ENGINE CONTROLLER APPARATUSES, METHODS AND SYSTEMS 审中-公开
公开(公告)号：US20170243496A1
公开(公告)日：2017-08-24
申请号：US15427917
申请日：2017-02-08
申请人： Telvent DTN LLC
发明人： Donald MCCANN , James H. BLOCK , Daniel W. LENNARTSON
IPC分类号： G08G5/00
CPC分类号： G08G5/0091 , G08G5/0013 , G08G5/0021 , G08G5/0034 , G08G5/0039
摘要： The DYNAMIC TURBULENCE ENGINE CONTROLLER APPARATUSES, METHODS AND SYSTEMS (“DTEC”) transform weather, terrain, and flight parameter data via DTEC components into turbulence avoidance optimized flight plans. In one implementation, the DTEC comprises a processor and a memory disposed in communication with the processor and storing processor-issuable instructions to receive anticipated flight plan parameter data, obtain terrain data based on the flight plan parameter data, obtain atmospheric data based on the flight plan parameter data, and determine a plurality of four-dimensional grid points based on the flight plan parameter data. The DTEC may then determine a non-dimensional mountain wave amplitude and mountain top wave drag, an upper level non-dimensional gravity wave amplitude, and a buoyant turbulent kinetic energy. The DTEC determines a boundary layer eddy dissipation rate, storm velocity, and eddy dissipation rate from updrafts, maximum updraft speed at grid point equilibrium level and storm divergence while the updraft speed is above the equilibrium level and identify storm top. The DTEC determines storm overshoot and storm drag, Doppler speed, eddy dissipation rate above the storm top, and determine eddy dissipation rate from downdrafts. The DTEC then determines the turbulent kinetic energy for each grid point and identifies an at least one flight plan based on the flight plan parameter data and the determined turbulent kinetic energy.

69. 发明授权

US09741252B2 Flight management system and method for monitoring flight guidance instructions 有权
公开(公告)号：US09741252B2
公开(公告)日：2017-08-22
申请号：US14965509
申请日：2015-12-10
申请人： Airbus Operations (SAS)
发明人： Jean-Claude Mere , Mathieu Versini
IPC分类号： G05D1/00 , G08G5/00 , B64C13/18
CPC分类号： G08G5/0039 , B64C13/18 , G05D1/0077 , G08G5/0034 , G08G5/0047
摘要： A flight management assembly including two guidance systems, each one provided with a flight management system. The flight management systems are independent and hosted in different computer equipment. Each of the flight management systems being configured to carry out at least a computation of guidance commands for the aircraft. The flight management assembly also includes a monitoring unit hosted in computer equipment different from the computer equipment hosting the flight management systems and configured to monitor at least the guidance commands computed by the two flight management systems to detect and identify a defective flight management system.

70. 发明申请

US20170233071A1 System and Method for Return-Home Command in Manual Flight Control 审中-公开
公开(公告)号：US20170233071A1
公开(公告)日：2017-08-17
申请号：US15433967
申请日：2017-02-15
申请人： Skyyfish, LLC
发明人： Orest Jacob Pilskalns , Colin Brian Heidtman
IPC分类号： B64C39/02 , G07C5/00 , G08G5/00 , G05D1/00 , G05D1/10
CPC分类号： B64C39/024 , B64C2201/027 , B64C2201/141 , B64C2201/146 , G05D1/0011 , G05D1/0061 , G05D1/101 , G07C5/004 , G07C5/008 , G08G5/0013 , G08G5/0021 , G08G5/0039 , G08G5/0056 , G08G5/0069 , G08G5/025
摘要： A return-to-home command for securing an unmanned aerial vehicle (UAV) from flying away. Flight plan updates that may be uploaded to the UAV can be interrupted at any time by uploading a modified flight plan or by instructing the UAV to pause while manual flight commands are given. The modifications to the original flight plan always ensure that a return-to-home step is present in the instructions on board the UAV, so that if the radio communications link between the remote controller and the UAV is lost, the UAV will fly home.

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