Timer initiated convergence of a GNSS receiver
First Claim
Patent Images
1. A method of implementing GNSS convergence, said method comprising:
- shutting down a GNSS receiver, wherein the GNSS receiver is coupled with a GNSS antenna attached to a mobile machine, and wherein the GNSS receiver is in a converged state and the GNSS antenna is at a first location at shut down;
storing the first location of the GNSS antenna at shut down;
monitoring a movement sensor at a first time to determine whether a net movement of the GNSS antenna, while the GNSS receiver is shut down, exceeds a threshold net movement parameter;
determining a second time based on whether the net movement of the GNSS antenna, while the GNSS receiver is shut down, exceeds the threshold net movement parameter;
automatically powering up the GNSS receiver at the second time; and
upon power up of the GNSS receiver, automatically initiating a convergence algorithm for the GNSS receiver, wherein the convergence algorithm is selected from a first convergence algorithm and a second convergence algorithm, wherein the first convergence algorithm is selected upon determining that the net movement of the GNSS antenna, while the GNSS receiver is shut down, does not exceed the threshold net movement parameter, and the second convergence algorithm is selected upon determining that the net movement of the GNSS antenna, while the GNSS receiver is shut down, meets or exceeds the threshold net movement parameter, and wherein;
the first convergence algorithm comprises;
generating ionosphere-free phase observations based on code and phase observations received by the GNSS receiver upon power up;
generating ionosphere-free time delta phase observations based on the ionosphere-free phase observations, wherein integer ambiguity is cancelled in the ionosphere-free time delta phase observations;
generating least square estimations for minimizing a cost function, wherein the cost function is based on differences between the ionosphere-free time delta phase observations and modeled parameters derived from ephemeris satellite orbit and clock data received from a network of GNSS reference receivers, and wherein the least square estimations result in one or more values, each value representing a change of the GNSS antenna'"'"'s position in a respective time interval of (t−
1, t); and
estimating a current location of the GNSS antenna by obtaining a sum of the one or more values resulted from the least square estimations and adding the stored first location of the GNSS antenna at shut down to the sum; and
the second convergence algorithm comprises estimating the current location of the GNSS antenna using a carrier phase ambiguity resolution procedure based on the code and phase observations received by the GNSS receiver upon power up and the ephemeris satellite orbit and clock data received from the network of GNSS reference receivers.
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Abstract
A method of implementing convergence of a Global Navigation Satellite System (GNSS) receiver is disclosed. A GNSS receiver which is coupled with a mobile machine is shut down. The GNSS receiver is in a converged state at shut down. The GNSS receiver is automatically powered up at a preset time. A convergence algorithm is automatically initiated prior to start of work that utilizes the GNSS receiver.
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Citations
11 Claims
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1. A method of implementing GNSS convergence, said method comprising:
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shutting down a GNSS receiver, wherein the GNSS receiver is coupled with a GNSS antenna attached to a mobile machine, and wherein the GNSS receiver is in a converged state and the GNSS antenna is at a first location at shut down; storing the first location of the GNSS antenna at shut down; monitoring a movement sensor at a first time to determine whether a net movement of the GNSS antenna, while the GNSS receiver is shut down, exceeds a threshold net movement parameter; determining a second time based on whether the net movement of the GNSS antenna, while the GNSS receiver is shut down, exceeds the threshold net movement parameter; automatically powering up the GNSS receiver at the second time; and upon power up of the GNSS receiver, automatically initiating a convergence algorithm for the GNSS receiver, wherein the convergence algorithm is selected from a first convergence algorithm and a second convergence algorithm, wherein the first convergence algorithm is selected upon determining that the net movement of the GNSS antenna, while the GNSS receiver is shut down, does not exceed the threshold net movement parameter, and the second convergence algorithm is selected upon determining that the net movement of the GNSS antenna, while the GNSS receiver is shut down, meets or exceeds the threshold net movement parameter, and wherein; the first convergence algorithm comprises; generating ionosphere-free phase observations based on code and phase observations received by the GNSS receiver upon power up; generating ionosphere-free time delta phase observations based on the ionosphere-free phase observations, wherein integer ambiguity is cancelled in the ionosphere-free time delta phase observations; generating least square estimations for minimizing a cost function, wherein the cost function is based on differences between the ionosphere-free time delta phase observations and modeled parameters derived from ephemeris satellite orbit and clock data received from a network of GNSS reference receivers, and wherein the least square estimations result in one or more values, each value representing a change of the GNSS antenna'"'"'s position in a respective time interval of (t−
1, t); andestimating a current location of the GNSS antenna by obtaining a sum of the one or more values resulted from the least square estimations and adding the stored first location of the GNSS antenna at shut down to the sum; and the second convergence algorithm comprises estimating the current location of the GNSS antenna using a carrier phase ambiguity resolution procedure based on the code and phase observations received by the GNSS receiver upon power up and the ephemeris satellite orbit and clock data received from the network of GNSS reference receivers. - View Dependent Claims (2, 3)
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4. A non-transitory computer readable storage medium having computer readable instructions stored thereon for causing a computer system to perform a method of implementing convergence selection of a Global Navigation Satellite System (GNSS) receiver, the method comprising:
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shutting down the GNSS receiver, wherein the GNSS receiver is coupled with a GNSS antenna attached to a mobile machine, and wherein the GNSS receiver is in a converged state and the GNSS antenna is at a first location at shut down; storing the first location of the GNSS antenna at shut down; monitoring a movement sensor at a first time to determine whether a net movement of the GNSS antenna, while the GNSS receiver is shut down, exceeds a threshold net movement parameter; determining a second time based on whether the net movement of the GNSS antenna, while the GNSS receiver is shut down, exceeds the threshold net movement parameter; automatically powering up the GNSS receiver at the second time; and upon power up of the GNSS receiver, automatically initiating a convergence algorithm for the GNSS receiver, wherein the convergence algorithm is selected from a first convergence algorithm and a second convergence algorithm, wherein the first convergence algorithm is selected upon determining that the net movement of the GNSS antenna, while the GNSS receiver is shut down, does not exceed the threshold net movement parameter, and the second convergence algorithm is selected upon determining that the net movement of the GNSS antenna, while the GNSS receiver is shut down, meets or exceeds the threshold net movement parameter, and wherein; the first convergence algorithm comprises; generating ionosphere-free phase observations based on code and phase observations received by the GNSS receiver upon power up; generating ionosphere-free time delta phase observations based on the ionosphere-free phase observations, wherein integer ambiguity is cancelled in the ionosphere-free time delta phase observations; generating least square estimations for minimizing a cost function, wherein the cost function is based on differences between the ionosphere-free time delta phase observations and modeled parameters derived from ephemeris satellite orbit and clock data received from a network of GNSS reference receivers, and wherein the least square estimations result in one or more values, each value representing a change of the GNSS antenna'"'"'s position in a respective time interval of (t−
1, t); andestimating a current location of the GNSS antenna by obtaining a sum of the one or more values resulted from the least square estimations and adding the stored first location of the GNSS antenna at shut down to the sum; and the second convergence algorithm comprises estimating the current location of the GNSS antenna using a carrier phase ambiguity resolution procedure based on the code and phase observations received by the GNSS receiver upon power up and the ephemeris satellite orbit and clock data received from the network of GNSS reference receivers. - View Dependent Claims (5, 6)
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7. A navigation system comprising:
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a GNSS receiver coupled with a GNSS antenna attached to a mobile machine; a movement sensor configured to monitor movement of the GNSS antenna; and a processor configured to; cause the GNSS receiver to transition into a shut down state, wherein the GNSS receiver is at a converged state and the GNSS antenna is at a first location at shut down;
store the first location of the GNSS antenna at shut down;monitor the movement sensor at a first time to determine whether a net movement of the GNSS antenna, while the GNSS receiver is shut down, exceeds a threshold net movement parameter; determine a second time based on whether the net movement of the GNSS antenna, while the GNSS receiver is shut down, exceeds the threshold net movement parameter; automatically power up the GNSS receiver at the second time; and upon power up of the GNSS receiver, automatically initiate a convergence algorithm for the GNSS receiver, wherein the convergence algorithm is selected from a first convergence algorithm and a second convergence algorithm, wherein the first convergence algorithm is selected upon determining that the net movement of the GNSS antenna, while the GNSS receiver is shut down, does not exceed the threshold net movement parameter, and the second convergence algorithm is selected upon determining that the net movement of the GNSS antenna, while the GNSS receiver is shut down, meets or exceeds the threshold net movement parameter, and wherein; the first convergence algorithm comprises; generating ionosphere-free phase observations based on code and phase observations received by the GNSS receiver upon power up; generating ionosphere-free time delta phase observations based on the ionosphere-free phase observations, wherein integer ambiguity is cancelled in the ionosphere-free time delta phase observations; generating least square estimations for minimizing a cost function, wherein the cost function is based on differences between the ionosphere-free time delta phase observations and modeled parameters derived from ephemeris satellite orbit and clock data received from a network of GNSS reference receivers, and wherein the least square estimations result in one or more values, each value representing a change of the GNSS antenna'"'"'s position in a respective time interval of (t−
1, t); andestimating a current location of the GNSS antenna by obtaining a sum of the one or more values resulted from the least square estimations and adding the stored first location of the GNSS antenna at shut down to the sum; and the second convergence algorithm comprises estimating the current location of the GNSS antenna using a carrier phase ambiguity resolution procedure based on the code and phase observations received by the GNSS receiver upon power up and the ephemeris satellite orbit and clock data received from the network of GNSS reference receivers. - View Dependent Claims (8, 9, 10, 11)
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Specification