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1.发明授权Device, system and methods using angle of arrival measurements for ADS-B authentication and navigation 有权使用ADS-B认证和导航的到达角测量装置，系统和方法公开(公告)号：US09476962B2
公开(公告)日：2016-10-25
申请号：US13875749
申请日：2013-05-02
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy , William Matthew Harris
CPC classification number: G01S19/04 , G01S3/043 , G01S3/46 , G01S5/0072 , G01S5/021 , G01S5/08 , G01S19/215
Abstract: The present disclosure is directed to a receiver for Automatic Dependent Surveillance Broadcast (ADS-B) verification of a target aircraft including a first input for receiving flight tracking information from a target aircraft that indicates positional information of the target aircraft. The receiver further includes a second input for receiving positional and heading information indicating the location and orientation of a multi-element array antenna configured to be attached to the receiver, and a processing module that generates a measured bearing derived from angle of arrival data, and an expected bearing of the target aircraft derived from the indicated positional information of the target aircraft and the positional and heading information defining the receiver location and orientation. A comparator compares the expected bearing to the measured bearing and verifies the ADS-B flight tracking information of the target aircraft and outputs an indication of authenticity based on the verification.
Abstract translation: 本公开涉及用于目标飞行器的自动相关监视广播（ADS-B）验证的接收机，其包括用于从目标飞行器接收指示目标飞行器的位置信息的飞行跟踪信息的第一输入。 接收机还包括第二输入端，用于接收指示被配置为附接到接收机的多元件阵列天线的位置和方向的位置和方位信息;以及处理模块，其生成从到达数据数据得到的测量轴承，以及 从目标飞行器的指示的位置信息得到的目标飞行器的预期方位和定义接收机位置和方向的位置和航向信息。 比较器将预期方向与测量方位进行比较，并验证目标飞机的ADS-B航班跟踪信息，并根据验证输出真实性指示。
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Patent Agency Ranking
公开(公告)号：US10365374B2
公开(公告)日：2019-07-30
申请号：US15234451
申请日：2016-08-11
Applicant: THE BOEING COMPANY
Inventor： Timothy Allen Murphy , William Matthew Harris
Abstract: The present disclosure is directed to a receiver for Automatic Dependent Surveillance Broadcast (ADS-B) verification of a target aircraft including a first input for receiving flight tracking information from a target aircraft that indicates positional information of the target aircraft. The receiver further includes a second input for receiving positional and heading information indicating the location and orientation of a multi-element array antenna configured to be attached to the receiver, and a processing module that generates a measured bearing derived from angle of arrival data, and an expected bearing of the target aircraft derived from the indicated positional information of the target aircraft and the positional and heading information defining the receiver location and orientation. A comparator compares the expected bearing to the measured bearing and verifies the ADS-B flight tracking information of the target aircraft and outputs an indication of authenticity based on the verification.
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3.发明申请Device, System and Methods Using Angle of Arrival Measurements for ADS-B Authentication and Navigation 有权使用ADS-B认证和导航到达角度的设备，系统和方法公开(公告)号：US20140327581A1
公开(公告)日：2014-11-06
申请号：US13875749
申请日：2013-05-02
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy , William Matthew Harris
IPC: G01S3/04
CPC classification number: G01S19/04 , G01S3/043 , G01S3/46 , G01S5/0072 , G01S5/021 , G01S5/08 , G01S19/215
Abstract: The present disclosure is directed to a receiver for Automatic Dependent Surveillance Broadcast (ADS-B) verification of a target aircraft including a first input for receiving flight tracking information from a target aircraft that indicates positional information of the target aircraft. The receiver further includes a second input for receiving positional and heading information indicating the location and orientation of a multi-element array antenna configured to be attached to the receiver, and a processing module that generates a measured bearing derived from angle of arrival data, and an expected bearing of the target aircraft derived from the indicated positional information of the target aircraft and the positional and heading information defining the receiver location and orientation. A comparator compares the expected bearing to the measured bearing and verifies the ADS-B flight tracking information of the target aircraft and outputs an indication of authenticity based on the verification.
Abstract translation: 本公开涉及用于目标飞行器的自动相关监视广播（ADS-B）验证的接收机，其包括用于从目标飞行器接收指示目标飞行器的位置信息的飞行跟踪信息的第一输入。 接收机还包括第二输入端，用于接收指示被配置为附接到接收机的多元件阵列天线的位置和方向的位置和方位信息;以及处理模块，其生成从到达数据数据得到的测量轴承，以及 从目标飞行器的指示的位置信息得到的目标飞行器的预期方位和定义接收机位置和方向的位置和航向信息。 比较器将预期方向与测量方位进行比较，并验证目标飞机的ADS-B航班跟踪信息，并根据验证输出真实性指示。
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公开(公告)号：US11163067B2
公开(公告)日：2021-11-02
申请号：US16838990
申请日：2020-04-02
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy , William Matthew Harris , Janet Suzanne Booth
Abstract: An interface device that enables a GNSS-based precision approach through the Ground Base Augmentation System (GBAS) function known as the GNSS Landing System (GLS) and/or through Satellite Based Augmentation Systems (SBAS) based Localizer Performance with Vertical Guidance (LPV). The GLS interface device allows a GLS-capable multi-mode receiver to be used on a non-GLS-capable airplane without extensive changes to other airplane systems. The GLS interface device works by intercepting information to and from the multi-mode receiver and modifying the information to make the interface compatible with an airplane that uses ILS guidance. Similarly, the information modifications will make the airplane appear to the multi-mode receiver as if it were a GLS-capable airplane.
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公开(公告)号：US20210311200A1
公开(公告)日：2021-10-07
申请号：US16838990
申请日：2020-04-02
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy , William Matthew Harris , Janet Suzanne Booth
Abstract: An interface device that enables a GNSS-based precision approach through the Ground Base Augmentation System (GBAS) function known as the GNSS Landing System (GLS) and/or through Satellite Based Augmentation Systems (SBAS) based Localizer Performance with Vertical Guidance (LPV). The GLS interface device allows a GLS-capable multi-mode receiver to be used on a non-GLS-capable airplane without extensive changes to other airplane systems. The GLS interface device works by intercepting information to and from the multi-mode receiver and modifying the information to make the interface compatible with an airplane that uses ILS guidance. Similarly, the information modifications will make the airplane appear to the multi-mode receiver as if it were a GLS-capable airplane.
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公开(公告)号：US20200371245A1
公开(公告)日：2020-11-26
申请号：US16420529
申请日：2019-05-23
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy , William Matthew Harris
Abstract: A satellite navigation system including a digital controlled reception pattern antenna (DCRPA) subsystem and a global navigation satellite system (GNSS) receiver. The overall system is designed so that all radio frequency (RF) processing and digital sampling are incorporated in the DCRPA subsystem. The RF signal from each element of the DCRPA array is digitized separately. Then the resultant digital samples are combined into a single bit stream which is transmitted to the GNSS receiver. Preferably the GNSS receiver is a software defined radio. The arrangement allows the DCRPA subsystem and the GNSS receiver to be connected with a single coaxial cable. Such an arrangement would allow simple retrofit of CRPA antennas to existing airframe designs as well as simple and inexpensive installations on new aircraft designs.
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