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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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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：US20230315930A1
公开(公告)日：2023-10-05
申请号：US17721912
申请日：2022-04-15
Applicant: Reliable Robotics Corporation
Inventor： Jonathan Dring , Robert J. Briody , Christopher Schulenberg
CPC classification number: G06F30/15 , G06F30/12 , G06F2111/02
Abstract: System and graphical user interface for generating reference data objects that include a reference to immutable expectation content for an aircraft expectation file. Reference data objects are allocated to nodes of an allocation tree data structure which are referenced during creation of requirement data objects. Requirement data objects capture engineering requirement content for a portion of the aircraft and a link to one or more corresponding reference data objects from which immutable expectation content may be viewed through selection of the link. The systems and methods can be used to efficiently and accurately audit a set of requirements specified for a given aircraft with respect to a set of aircraft expectation files.
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Patent Agency Ranking
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：US12162586B2
公开(公告)日：2024-12-10
申请号：US18097109
申请日：2023-01-13
Applicant: Reliable Robotics Corporation
Inventor： David DeHaan
Abstract: An aircraft may include a control lever movable along a lever path and configured to control a system of the aircraft, and a selectively engageable detent feature configured to inhibit travel of the control lever and operable in a disengaged configuration in which the control lever is movable along the lever path without restriction by the selectively engageable detent feature, and an engaged configuration in which the selectively engageable detent feature inhibits travel of the control lever at a particular location along the lever path.
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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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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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