Invention Grant
- Patent Title: Concurrent, multi-sensor, multi-inertial navigation system flight emulation
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Application No.: US17235564Application Date: 2021-04-20
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Publication No.: US11756433B2Publication Date: 2023-09-12
- Inventor: Brad S. Williams , Thomas M. Taylor
- Applicant: Raytheon Company
- Applicant Address: US MA Waltham
- Assignee: Raytheon Company
- Current Assignee: Raytheon Company
- Current Assignee Address: US MA Waltham
- Agency: Schwegman Lundberg & Woessner, P.A.
- Main IPC: G08G5/00
- IPC: G08G5/00 ; B64D43/02 ; G01C21/20 ; G01S19/45 ; G05D1/10

Abstract:
A flight emulation system receives global positioning system (GPS) data into one or more EGIs (embedded GPS/inertial navigation system (INS)) or GPS receivers from a GPS emulator. The GPS data are based on a pre-defined flight trajectory plan of an aircraft. The system calculates real-time positional, orientational, and inertial emulation data using outputs of the EGIs or GPS receivers and platform-specific, flight dynamics data, and then transmits the real-time positional, orientational, and inertial emulation data to one or more subsystems associated with the aircraft for use by operations of the one or more subsystems.
Public/Granted literature
- US20220335836A1 CONCURRENT, MULTI-SENSOR, MULTI-INERTIAL NAVIGATION SYSTEM FLIGHT EMULATION Public/Granted day:2022-10-20
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