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公开(公告)号：US20240363015A1
公开(公告)日：2024-10-31
申请号：US18341145
申请日：2023-06-26
发明人： Anoop S , Mohammed Ibrahim Mohideen
CPC分类号： G08G5/065 , G08G5/0021 , G08G5/003 , G08G5/045
摘要： Systems and methods are provided for promoting intersection takeoff awareness. The system includes a database storing runway data that includes identifications and locations of runways, identifications and locations of intersections along the runways, and lengths of the runways, a sensor system configured to generate aircraft position data that includes a current position of the aircraft, a display device, and a controller configured to, by a processor: retrieve the runway data, receive the aircraft position data, identify a first intersection of a first runway as the aircraft approaches the first intersection, determine a runway distance available from the first intersection, and display, on the display device, prior to the aircraft entering the first runway, the runway distance from the first intersection and/or an indication as to whether the runway distance from the first intersection is sufficient for takeoff based on performance parameters of the aircraft and safe takeoff criteria.
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公开(公告)号：US20180247548A1
公开(公告)日：2018-08-30
申请号：US15443168
申请日：2017-02-27
CPC分类号： G08G5/0091 , B64D43/00 , G01C23/00 , G06T11/60 , G08G5/0013 , G08G5/0021 , G08G5/003 , G08G5/0052 , H04B7/18506 , H04W84/005
摘要： A method of supplementing high design assurance level system information for an aircraft is provided. The method includes dynamically gathering low design assurance level information from the internet with a communication system based on a requests by a cockpit browser. The low design assurance level information is parsed with the high design assurance level information with a parser of the cockpit browser to generate combined assurance level information. The combined assurance level information is displayed on a display.
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公开(公告)号：US10460612B2
公开(公告)日：2019-10-29
申请号：US15823867
申请日：2017-11-28
发明人： Nathan K , Anoop S , Sabu Mathew
摘要： Methods and systems for flight control of a supersonic ownship are provided. The systems utilize sources of weather data, a flight management system (FMS) of the supersonic ownship, and sources of neighbor traffic data. The systems generate a complete neighbor traffic flight trajectory, and then process the complete neighbor traffic flight trajectory with a flight plan of the supersonic ownship, aircraft specific parameters, and forecasted and real-time weather data to generate therefrom a safe sonic altitude for flying the supersonic ownship. The safe sonic altitude is transmitted to air traffic control (ATC) as a request for an assignment. Upon receiving the assignment from ATC, the systems notify the pilot of the assignment and continue monitoring airspace for real-time changes in the flight path trajectory of the neighbor traffic. The sonic altitude is updated based on a detected real-time change in the flight path trajectory of the neighbor traffic.
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公开(公告)号：US10176721B2
公开(公告)日：2019-01-08
申请号：US15370029
申请日：2016-12-06
发明人： Pramod Kumar Malviya , Pradeep Huncha , Vinay Somashekar , Sreenivasan Govindillam K , Nathan K , Anoop S , Sunitha Panchangam
摘要： Systems and methods are provided for displaying portions of a route on a coverage map that are non-compliant for a Global Navigation Satellite System (GNSS) navigation system in an aircraft. A route compliance module defines a geodetic reference datum standard based on the GNSS navigation system. A navigation system database has compliance information corresponding to each of a plurality of airports. A flight management system determines the route of the aircraft and a visual display displays the route and the coverage map. The route compliance module identifies a non-compliant region of the coverage map that is not compliant with the geodetic reference datum standard based on the compliance information and adjusts the visual display to differentiate a non-compliant portion of the route extending within the non-compliant region of the coverage map.
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公开(公告)号：US09752893B2
公开(公告)日：2017-09-05
申请号：US14813957
申请日：2015-07-30
CPC分类号： G01C23/005 , B64D45/04 , G05D1/0684 , G06K9/00637 , G08G5/0021 , G08G5/025
摘要： A display system for an aircraft includes a sensor configured to capture data associated with a landing platform on a movable carrier. The data includes current energy parameters of the movable carrier. The display system further includes a processing unit configured to receive the data representative of the landing platform. The processing unit is further configured to generate display commands associated with the landing platform. The display system further includes a display device coupled the processing unit for receiving the display commands and operable to render first symbology representing the landing platform.
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公开(公告)号：US11670181B2
公开(公告)日：2023-06-06
申请号：US17062781
申请日：2020-10-05
发明人： Anoop S , Mohammed Ibrahim Mohideen , Gang He
摘要： The present disclosure relates to a vertical takeoff and landing, VTOL, vehicle having a landing aid and associated methods. The landing aid includes at least one processor is configured to: receive image data from an image capture device, receive altitude data from the altimeter, retrieve template landing pad image data for a target landing pad from the database, scale the template landing pad image data based on the altitude data, compare the scaled template landing pad image data and the image data received from the image capture device to locate the target landing pad therein, thereby providing target landing pad localization data, and control a function of the VTOL vehicle based on the target landing pad localization data.
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7.发明授权公开(公告)号：US10762793B2
公开(公告)日：2020-09-01
申请号：US16101678
申请日：2018-08-13
摘要： Systems and methods for selecting a runway record for a target runway are provided. The system includes: a first database having a first runway record with a first runway threshold; a second database having a second runway record with a second runway threshold; a transceiver for receiving an ILS signal; and a computer system. The computer system is configured to determine when the ILS signal is substantially zero. When the ILS signal is substantially zero, the computer system is configured to receive, from one or more databases, a plurality of runway records including corresponding runway thresholds; and select a most accurate runway record from the plurality of runway records based, at least in part, on which of the corresponding runway thresholds deviates least from the aiming point. In various embodiments, the most accurate runway record is then utilized for rendering images in a cockpit display system.
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8.发明申请SYSTEM AND METHOD FOR AIDING A PILOT IN LOCATING AN OUT OF VIEW LANDING SITE 有权用于寻找位于不正确的露天场地的导弹的系统和方法公开(公告)号：US20160152348A1
公开(公告)日：2016-06-02
申请号：US14558195
申请日：2014-12-02
CPC分类号： G01C21/00 , G01C23/005 , G05D1/0202 , G05D1/0676
摘要： A system and method for displaying symbology that is indicative of the direction of a landing site is provided. The provided system and method generate and display, prior to the rotorcraft reaching the MAP, symbology that conveys visual guidance that may be quickly and easily comprehended by a pilot. The provided system and method reduce the pilot's visual scan area and associated search time, reducing cognitive workload and increasing situational awareness.
摘要翻译： 提供了一种用于显示指示着陆站点方向的符号系统和方法。 提供的系统和方法在旋翼航空器到达MAP之前生成和显示，传达视觉指导的符号体系，可以快速轻松地被飞行员理解。 提供的系统和方法减少了飞行员的视觉扫描区域和相关的搜索时间，减少了认知工作量并增加了情境意识。
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公开(公告)号：US20220348350A1
公开(公告)日：2022-11-03
申请号：US17352526
申请日：2021-06-21
发明人： Anoop S , Mohammed Ibrahim Mohideen
摘要： Methods and systems are provided for displaying multiple time rings on an avionic display. The method includes displaying at least a first time ring in an avionic display; displaying at least a second time ring in the avionic display wherein the first and second time rings include a pair of visually spaced apart time rings wherein a visual spacing apart between the first and second time rings is indicative of a range and a separation flight time between each of the time rings; and displaying, about at least the first time ring in the avionic display, a distance marker of a value for a range and a time marker of a value for separation flight time about an ownship's position and airspeed, and to at least one time ring.
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10.发明申请公开(公告)号：US20210343159A1
公开(公告)日：2021-11-04
申请号：US16904227
申请日：2020-06-17
发明人： Sanju Kuriakose , Anoop S , Sabu Mathew , Niranjan Kumar , Jan Hart , Janaki Seetharaman
摘要： A system for automatically constructing a flight plan that aligns with a boundary line is provided. The system has a controller that is configured to: automatically select a set of geographical (geo) coordinate waypoints along a boundary line using waypoints from the geographical database responsive to flight crew input; refine the set of geo coordinate waypoints using a calculated turn initiation distance and a turn completion distance for every waypoint; further refine the refined set of geo coordinate waypoints based on the course change between waypoints; generate a set of courses and distances between waypoints through computing, for each set of two consecutive waypoints in the further refined set of geo coordinate waypoints, the course and distance between the two consecutive waypoints; and construct the flight plan based on the waypoints in the further refined set of geo coordinate waypoints and the set of courses and distances between waypoints.
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