REAL-TIME HIGH ACCURACY POSITION AND ORIENTATION SYSTEM
First Claim
1. A system comprising:
- a GNSS receiver, configured for use on a vehicle, to generate GNSS position data indicative of approximate positions of the vehicle during a data acquisition period in which the vehicle is in motion; and
an integrated inertial navigation (IIN) module, configured for use on the vehicle, to execute an RTK algorithm during the data acquisition period to generate output position data indicative of positions of the vehicle at a greater precision than the GNSS position data, based on the GNSS position data, inertial measurement data acquired on the vehicle during the data acquisition period, and a set of VRS observables received during the data acquisition period from a remote source that is external to the vehicle, where the VRS observables are based on the GNSS position data.
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Accused Products
Abstract
A real-time high accuracy position and orientation system (RT-HAPOS) system for a vehicle, such as an aircraft, comprises a global navigation satellite system (GNSS) receiver disposed on the vehicle and an integrated inertial navigation (IIN) module disposed on the vehicle. The GNSS receiver generates GNSS position data indicating approximate positions of the vehicle during a data acquisition period in which the vehicle is moving. The IIN module executes a real-time kinematic (RTK) algorithm during the data acquisition period to generate output position data indicating positions of the vehicle at a greater precision than the GNSS position data, based on the GNSS position data, inertial measurement data acquired on the vehicle during the data acquisition period, and a set of virtual reference station (VRS) observables received during the data acquisition period from a remote source external to the vehicle, where the VRS observables are based on the GNSS position data.
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Citations
25 Claims
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1. A system comprising:
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a GNSS receiver, configured for use on a vehicle, to generate GNSS position data indicative of approximate positions of the vehicle during a data acquisition period in which the vehicle is in motion; and an integrated inertial navigation (IIN) module, configured for use on the vehicle, to execute an RTK algorithm during the data acquisition period to generate output position data indicative of positions of the vehicle at a greater precision than the GNSS position data, based on the GNSS position data, inertial measurement data acquired on the vehicle during the data acquisition period, and a set of VRS observables received during the data acquisition period from a remote source that is external to the vehicle, where the VRS observables are based on the GNSS position data. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. A positioning system for a vehicle, comprising:
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an inertial navigation module to generate an inertial navigation solution for the vehicle based on inertial sensor data; a filter to input the inertial navigation solution and aiding sensor data including rover GNSS data generated on the vehicle, and further to input VRS GNSS data transmitted to the vehicle from a remote source, the filter further to estimate floated carrier phase ambiguities in combinations of rover carrier phase observables and VRS carrier phase observables from the rover GNSS data and the VRS GNSS data; and an ambiguity resolution module to determine integer ambiguities from the floated ambiguity data and to output the integer ambiguities to the filter; the filter further to generate and output a position solution for the vehicle based on the integer ambiguities. - View Dependent Claims (10, 11, 12, 13)
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14. A georeferencing system comprising:
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a GNSS receiver, disposed on an aircraft, to generate GNSS position data indicative of approximate positions of an aircraft during a data acquisition period; a transmitter, disposed on the aircraft, to transmit, during the data acquisition period, the GNSS position data to a remote source that is external to the aircraft; a receiver, disposed on the aircraft, to receive during the data acquisition period a set of VRS observables from the remote source, the VRS observables having been computed based on the GNSS data; an integrated inertial navigation (IIN) module, disposed on the aircraft, to input the GNSS position data and inertial measurement data acquired on the aircraft during the data acquisition period, and further to input during the data acquisition period the VRS observables, the IIN module further to acquire differential GNSS observables measurements and to perform integer carrier phase ambiguity resolution and carrier phase measurements during the data acquisition period, and to generate output position data indicative of precise positions of the aircraft based on the VRS observables, the GNSS position data and the inertial measurement data; a data acquisition device, disposed on the aircraft, to acquire data about features that are external to the vehicle, during the data acquisition period; and a processor, disposed on the aircraft, to georeference the data about features that are external to the vehicle with the output position data. - View Dependent Claims (15, 16)
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17. A system comprising:
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means disposed on a vehicle for obtaining differential GNSS observables measurements; means disposed on the vehicle for obtaining carrier phase measurements and for performing integer carrier phase ambiguity resolution; and means for integrating observables measurements from a plurality of fixed GNSS reference receivers arranged in a network to correct for atmospheric delays in the differential GNSS observables measurements when a minimum distance between the vehicle and the nearest one of the reference receivers to the vehicle exceeds a predetermined distance. - View Dependent Claims (18, 19)
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20. A method comprising:
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on a vehicle, obtaining differential GNSS observables measurements; on the vehicle, obtaining carrier phase measurements and for performing integer carrier phase ambiguity resolution; and on the vehicle, integrating observables measurements from a plurality of fixed GNSS reference receivers arranged in a network around the vehicle to correct for atmospheric delays in the differential GNSS observables measurements when a minimum distance between the vehicle and the nearest one of the reference receivers to the vehicle exceeds a predetermined distance. - View Dependent Claims (21, 22)
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23. A method of georeferencing data, the method comprising:
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obtaining GNSS position data indicative of approximate positions of the aircraft during a data acquisition period; transmitting, during the data acquisition period, the GNSS position data to a remote source that is external to the aircraft; receiving, during the data acquisition period, a set of VRS observables from the remote source, the VRS observables having been computed based on the GNSS data; performing integer carrier phase ambiguity resolution and carrier phase measurements during the data acquisition period to generate output position data indicative of precise positions of the aircraft based on the VRS observables, the GNSS position data and the inertial measurement data; using a data acquisition device to acquire data about features that are external to the aircraft, during the data acquisition period; and georeferencing the data about features that are external to the aircraft with the output position data. - View Dependent Claims (24, 25)
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Specification