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公开(公告)号：US20210027639A1
公开(公告)日：2021-01-28
申请号：US17067392
申请日：2020-10-09
Applicant: Reliable Robotics Corporation
Inventor： Robert W. Rose , Matthew T. Nehrenz , John P. Couluris , Juerg Frefel
Abstract: A system having components coupled to an aircraft and components remote from the aircraft processes radar-augmented data, transmits information between aircraft system components and/or remote system components, and dynamically determines locations and states of the aircraft, while the aircraft is in flight. Based on the locations and states of the aircraft, the system generates instructions for flight control of the aircraft toward a flight path appropriate to the locations of the aircraft, and can update flight control instructions as new data is received and processed.
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公开(公告)号：US11749126B2
公开(公告)日：2023-09-05
申请号：US17168190
申请日：2021-02-05
Applicant: Reliable Robotics Corporation
Inventor： Robert W. Rose , Matthew T. Nehrenz , John P. Couluris , Juerg Frefel
CPC classification number: G08G5/025 , B64D45/08 , B64D47/08 , G06T3/4015 , G06T7/70 , G06V20/176 , G08G5/0013 , G08G5/0026 , H04N5/33 , G06T2207/10021 , G06T2207/10032 , G06T2207/30241
Abstract: A system having components coupled to an aircraft and components remote from the aircraft processes sensor-derived data, transmits information between aircraft system components and remote system components, and dynamically generates updated analyses of position and orientation of the aircraft relative to a desired landing site, while the aircraft is in flight toward the desired landing site. Based on the position and orientation information, the system generates instructions for flight control of the aircraft toward a flight path to the landing site, and can update flight control instructions as new data is received and processed.
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公开(公告)号：US20200312170A1
公开(公告)日：2020-10-01
申请号：US16830008
申请日：2020-03-25
Applicant: Reliable Robotics Corporation
Inventor： Michael Andrew Sherback , Robert W. Rose , Matthew T. Nehrenz , John P. Couluris
Abstract: A system having components coupled to an aircraft in operation processes sensor-derived data, performs a localization cross-checking procedure, and dynamically generates updated analyses of the position and orientation of the aircraft. Based on the updated analyses, the system can generate instructions for flight control of the aircraft and can update flight control instructions as new data is received and processed. The system functions to reduce the “worst-case” bounds on a localization estimate for the aircraft to a low enough level that is appropriate for completing a flight operation.
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公开(公告)号：US12153148B2
公开(公告)日：2024-11-26
申请号：US17538671
申请日：2021-11-30
Applicant: Reliable Robotics Corporation
Inventor： Robert W. Rose , Matthew T. Nehrenz , Samuel P. Pullen
Abstract: An aircraft receives pseudorange input from a plurality of satellites of an augmentation system. Each pseudorange input includes a precise position solution and error data. The aircraft receives a high frequency measurement from an inertial navigation system. The aircraft applies the precise position solution, error data, and high frequency measurement to a set of parallel Schmidt extended Kalman filters to produce a corrected position solution and integrity data. The aircraft applies the integrity data to a receiver autonomous integrity monitoring system to produce a protection level for the corrected position solution. The aircraft performs an aircraft operation using the corrected position solution and protection level.
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公开(公告)号：US11928976B2
公开(公告)日：2024-03-12
申请号：US16830008
申请日：2020-03-25
Applicant: Reliable Robotics Corporation
Inventor： Michael Andrew Sherback , Robert W. Rose , Matthew T. Nehrenz , John P. Couluris
CPC classification number: G08G5/025 , B64D47/08 , G01C5/005 , G07C5/0808 , G08G5/0013 , G08G5/0021 , H04L9/0872
Abstract: A system having components coupled to an aircraft in operation processes sensor-derived data, performs a localization cross-checking procedure, and dynamically generates updated analyses of the position and orientation of the aircraft. Based on the updated analyses, the system can generate instructions for flight control of the aircraft and can update flight control instructions as new data is received and processed. The system functions to reduce the “worst-case” bounds on a localization estimate for the aircraft to a low enough level that is appropriate for completing a flight operation.
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Patent Agency Ranking
公开(公告)号：US20220365222A1
公开(公告)日：2022-11-17
申请号：US17538657
申请日：2021-11-30
Applicant: Reliable Robotics Corporation
Inventor： Robert W. Rose , Matthew T. Nehrenz , Samuel P. Pullen
Abstract: An aircraft receives pseudorange input from a plurality of satellites of an augmentation system. Each pseudorange input includes a precise position solution and error data. The aircraft receives a high frequency measurement from an inertial navigation system. The aircraft applies the precise position solution, error data, and high frequency measurement to a set of parallel Schmidt extended Kalman filters to produce a corrected position solution and integrity data. The aircraft applies the integrity data to a receiver autonomous integrity monitoring system to produce a protection level for the corrected position solution. The aircraft performs an aircraft operation using the corrected position solution and protection level.
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公开(公告)号：US12153147B2
公开(公告)日：2024-11-26
申请号：US17538657
申请日：2021-11-30
Applicant: Reliable Robotics Corporation
Inventor： Robert W. Rose , Matthew T. Nehrenz , Samuel P. Pullen
Abstract: An aircraft receives pseudorange input from a plurality of satellites of an augmentation system. Each pseudorange input includes a precise position solution and error data. The aircraft receives a high frequency measurement from an inertial navigation system. The aircraft applies the precise position solution, error data, and high frequency measurement to a set of parallel Schmidt extended Kalman filters to produce a corrected position solution and integrity data. The aircraft applies the integrity data to a receiver autonomous integrity monitoring system to produce a protection level for the corrected position solution. The aircraft performs an aircraft operation using the corrected position solution and protection level.
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公开(公告)号：US20210319709A1
公开(公告)日：2021-10-14
申请号：US17168190
申请日：2021-02-05
Applicant: Reliable Robotics Corporation
Inventor： Robert W. Rose , Matthew T. Nehrenz , John P. Couluris , Juerg Frefel
Abstract: A system having components coupled to an aircraft and components remote from the aircraft processes sensor-derived data, transmits information between aircraft system components and remote system components, and dynamically generates updated analyses of position and orientation of the aircraft relative to a desired landing site, while the aircraft is in flight toward the desired landing site. Based on the position and orientation information, the system generates instructions for flight control of the aircraft toward a flight path to the landing site, and can update flight control instructions as new data is received and processed.
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公开(公告)号：US20200050217A1
公开(公告)日：2020-02-13
申请号：US16057704
申请日：2018-08-07
Applicant: Reliable Robotics Corporation
Inventor： Robert W. Rose , Matthew T. Nehrenz , John P. Couluris , Juerg Frefel
Abstract: A system having components coupled to an aircraft and components remote from the aircraft processes sensor-derived data, transmits information between aircraft system components and remote system components, and dynamically generates updated analyses of position and orientation of the aircraft relative to a desired landing site, while the aircraft is in flight toward the desired landing site. Based on the position and orientation information, the system generates instructions for flight control of the aircraft toward a flight path to the landing site, and can update flight control instructions as new data is received and processed.
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公开(公告)号：US20240321124A1
公开(公告)日：2024-09-26
申请号：US18429947
申请日：2024-02-01
Applicant: Reliable Robotics Corporation
Inventor： Michael Andrew Sherback , Robert W. Rose , Matthew T. Nehrenz , John P. Couluris
CPC classification number: G08G5/025 , B64D47/08 , G01C5/005 , G07C5/0808 , G08G5/0013 , G08G5/0021 , H04L9/0872
Abstract: A system having components coupled to an aircraft in operation processes sensor-derived data, performs a localization cross-checking procedure, and dynamically generates updated analyses of the position and orientation of the aircraft. Based on the updated analyses, the system can generate instructions for flight control of the aircraft and can update flight control instructions as new data is received and processed. The system functions to reduce the “worst-case” bounds on a localization estimate for the aircraft to a low enough level that is appropriate for completing a flight operation.
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