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公开(公告)号：US20230359197A1
公开(公告)日：2023-11-09
申请号：US18222634
申请日：2023-07-17
Applicant: Reliable Robotics Corporation
Inventor： Robert W. Rose , Matthew T. Nehrenz , John P. Couluris , Juerg Frefel
CPC classification number: G05D1/0038 , B64D47/08 , G05D1/101
Abstract: While an aircraft is in flight toward the desired landing site, the aircraft generates a navigation solution to land the aircraft at the landing site. The navigation solution is transmitted to an operator that is at a location remote from the aircraft. The operator reviews the navigation solution and provides a confirmation whether the navigation solution is accurate back to the aircraft.
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公开(公告)号：US11763687B2
公开(公告)日：2023-09-19
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
CPC classification number: G08G5/0086 , G01S13/882 , G01S19/47 , G08G5/0039
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：US20220365224A1
公开(公告)日：2022-11-17
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：US10935987B2
公开(公告)日：2021-03-02
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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