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公开(公告)号：US20160090193A1
公开(公告)日：2016-03-31
申请号：US14497565
申请日：2014-09-26
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Gang He , Steve Johnson , Thea L. Feyereisen
CPC classification number: B64D45/04 , G08G5/0021 , G08G5/025
Abstract: A system and method are disclosed for indicating to an aircrew of an aircraft an unstable approach to a desired landing. When the energy state of the aircraft exceeds a threshold, a suggested airspeed in consideration of the energy state is displayed. Additionally, a landing spots on a displayed runway are shown indicating where the aircraft would land in view of the energy state and where the aircraft is recommended to land in view of the current aircraft type and weight. A text message may also be displayed that conveys the ability of the aircraft to land.
Abstract translation: 公开了一种系统和方法，用于向飞机的机组人员指示对期望着陆的不稳定方法。 当飞行器的能量状态超过阈值时，显示考虑能量状态的建议空速。 另外，显示的跑道上的着陆点被示出表明飞机将考虑到能量状态而降落在哪里，并且考虑到目前的飞机类型和重量，飞机被推荐降落在哪里。 还可以显示一条传达航空器着陆能力的短信。
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22.发明申请公开(公告)号：US20150211883A1
公开(公告)日：2015-07-30
申请号：US14164661
申请日：2014-01-27
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Gang He
CPC classification number: G01C23/005 , B64D43/02 , G05D1/0858 , G05D1/102 , G08B5/36 , G08G5/025
Abstract: An apparatus and method are provided for displaying a predicted image for rotocraft flight in consideration of data associated with a selected flight procedure and a current image.
Abstract translation: 提供了一种装置和方法，用于考虑与所选择的飞行过程和当前图像相关联的数据来显示用于旋转飞行的预测图像。
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23.发明申请公开(公告)号：US20140288733A1
公开(公告)日：2014-09-25
申请号：US13847151
申请日：2013-03-19
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Gang He , Ivan Sandy Wyatt
Abstract: Systems and methods for reducing error detection latency in LPV approaches are provided. In certain embodiments, a method for navigational guidance includes calibrating inertial measurements acquired from an inertial navigation system with satellite-based augmentation system position measurements acquired from a satellite-based augmentation system to create corrected inertial navigation system positions. The method also includes determining whether the satellite-based augmentation system experienced a fault when the inertial measurements were calibrated with the satellite-based augmentation system position measurements. Further, when the satellite-based augmentation system did not experience a fault, the method includes monitoring the satellite-based augmentation system navigation position measurements based on the corrected inertial navigation system positions.
Abstract translation: 提供了用于减少LPV方法中的错误检测延迟的系统和方法。 在某些实施例中，用于导航指导的方法包括校准从惯性导航系统获得的惯性测量，其具有从基于卫星的增强系统获取的基于卫星的增强系统位置测量值，以创建校正的惯性导航系统位置。 该方法还包括当使用基于卫星的增强系统位置测量校准惯性测量时，确定基于卫星的增强系统是否经历故障。 此外，当基于卫星的增强系统没有遇到故障时，该方法包括基于校正的惯性导航系统位置监视基于卫星的增强系统导航位置测量。
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24.发明申请METHOD AND APPARATUS FOR GENERATING A VIRTUAL INNER MARKER FOR AN AIRCRAFT LANDING APPROACH 有权用于生成虚拟内标用于航空器接地方法的方法和装置公开(公告)号：US20140222257A1
公开(公告)日：2014-08-07
申请号：US13759408
申请日：2013-02-05
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Ivan Sandy Wyatt , Gang He , Thea L. Feyereisen
IPC: B64D45/08
CPC classification number: B64D45/08 , G08G5/0021 , G08G5/02 , G08G5/025
Abstract: A system and method is disclosed for anticipating a missed approach point (MAP) during an instrument landing of an aircraft. Symbology is generated and displayed that graphically represents a lateral distance between a runway threshold and a virtual inner marker. The MAP is identified as the location of the aircraft when the symbology reaches a displayed runway threshold.
Abstract translation: 公开了一种用于在飞机的仪表着陆期间预期错过的接近点（MAP）的系统和方法。 生成和显示符号学，其以图形方式表示跑道阈值和虚拟内标记之间的横向距离。 当符号系统达到显示的跑道阈值时，MAP被标识为飞机的位置。
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25.发明申请公开(公告)号：US20250068178A1
公开(公告)日：2025-02-27
申请号：US18452860
申请日：2023-08-21
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Gang He
IPC: G05D1/46
Abstract: Systems and methods are provided for displaying roll rate on a vertical take-off and landing (VTOL) aircraft display. Aircraft roll data is received from at least one geospatial sensor of the VTOL aircraft. A roll rate scale associated with a desirable roll rate range of the VTOL aircraft is generated. An aircraft roll rate of the VTOL aircraft is determined based on the aircraft roll data. The VTOL aircraft display, including a graphical representation of the roll rate scale and the aircraft roll rate with respect to the roll rate scale, is generated for display on the display device.
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Patent Agency Ranking
公开(公告)号：US20240355214A1
公开(公告)日：2024-10-24
申请号：US18302367
申请日：2023-04-18
Applicant: HONEYWELL INTERNATIONAL INC.
CPC classification number: G08G5/0078 , B64D43/00 , B64D47/08 , G08G5/0021 , H04N7/185 , G01C23/00
Abstract: Systems and methods are provided for in-air traffic tracking onboard an ownship. The system includes a display device, a sensor system configured to sense a sensed three-dimensional (3D) position of a target aircraft, a communication system configured to receive in-air traffic position data from an external source that includes a tracked 3D position of the target aircraft, and an in-air traffic tracking system that includes a controller configured to, by a processor: determine a predicted 3D position of the target aircraft by adjusting the tracked 3D position with compensation parameters, wherein the compensation parameters are determined based on a trained machine learning, determine a real-time 3D position of the target aircraft based on the sensed 3D position and/or the predicted 3D position, and render a tracking icon on the display device that indicates the real-time 3D position of the target aircraft.
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27.发明申请公开(公告)号：US20230123419A1
公开(公告)日：2023-04-20
申请号：US17647191
申请日：2022-01-06
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Gang He , Zhihao Qin , Thea Feyereisen , Rakshit R
Abstract: Systems and methods for suggesting, on an avionic display in an aircraft, a communication frequency that is relevant to a context of the aircraft. The method includes determining a location and orientation of the aircraft and referencing an intended flight path to determine, based thereon, the context of the aircraft. The method uses the context to reference an on-board source of a plurality of stored navigation communication frequencies. The method identifies one or more relevant navigation communication frequencies for the context and presents the relevant navigation communication frequencies in a predefined area on an avionic display.
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公开(公告)号：US20230102215A1
公开(公告)日：2023-03-30
申请号：US17647261
申请日：2022-01-06
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea Feyereisen , Gang He , Abiram Rajendran , Ryan Milmoe
IPC: G06F3/04886 , G06F21/35 , G06F1/16 , H04W4/029
Abstract: Systems and methods for displaying a scorecard for rating pilot performance by registering a wearable device based on the identification of the wearable device through pilot profile data, location data, and an identification key data received from the wearable device; linking, the wearable device to the avionic system to receive flight data, and to a cloud server to receive computed performance scores for in-flight display by the wearable device; alternately, in response to a manual input action, authenticating pilot identity to enable pilot access and linking of the flight data to the cloud server for display; generating a set of flight components via a model specified for a flight phase based on data from the wearable device if available, and the flight data, the model includes flight performance score values; displaying a flight phase performance score; and displaying on the graphical user interface in a cockpit display the performance scorecard.
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公开(公告)号：US11574549B2
公开(公告)日：2023-02-07
申请号：US17112140
申请日：2020-12-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea Feyereisen , Rakshit R , Gang He
Abstract: Methods and systems are provided for guiding or otherwise assisting operation of an aircraft when diverting from a flight plan. One method involves determining a gliding trajectory for the aircraft based at least in part on a current altitude of the aircraft, providing a graphical representation of the gliding trajectory for the aircraft, identifying a plurality of landing locations within a range defined by the gliding trajectory from the aircraft, and for each landing location of the plurality of landing locations, providing a graphical representation of a respective landing location with respect to the gliding trajectory at a respective altitude associated with the respective landing location and at a respective distance with respect to a graphical representation of the aircraft corresponding to a respective geographic distance between a current location of the aircraft and the respective landing location.
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公开(公告)号：US11479365B2
公开(公告)日：2022-10-25
申请号：US17155983
申请日：2021-01-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Zhong Chen , Gang He , Min Wu , Carl Dins
Abstract: The present disclosure provides computer vision systems and methods for an aircraft. The computer vision systems and methods identify a runway based on video frame data from a camera mounted to the aircraft, extract runway pixel positions associated with the runway, determine the aircraft position in a real world coordinate frame based on the pixel positions, the aircraft position including an aircraft lateral position and an aircraft elevation, receive predefined aircraft position data and go-around rules for a compliant approach to the runway, calculate an aircraft position deviation based on the aircraft position and the predefined aircraft position data, determine whether the aircraft position deviation is in conformance with the go-around rules, and output an indication of conformity with the go-around rules.
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