Self-calibrating electronic distance measurement instrument
First Claim
1. A method of operating an electronic distance meter (EDM) subsystem of a total station, comprising the steps of:
- substantially continuously receiving from at least one orbiting GPS satellite radio signals with timing information controlled by an atomic clock on board said satellite;
constantly providing a global positioning system (GPS) receiver with a navigation computer for maintaining tracking of said radio signals and for deriving precise timing information from said radio signals;
persistently providing a local reference oscillator with a timing signal based on said derived precise time information;
permanently providing the EDM subsystem with a signal from said oscillator wherein said EDM subsystem sends an outbound laser signal to a distant target and receives an inbound signal reflected by said target;
measuring a difference between said out-bound signal and said resulting in-bound signal reflected from said distant surveyor target to determine the line-of-sight distance to said target;
wherein, the step of measuring provides a signal time-of-flight measurement with an accuracy derived from said precise timing information in said timing signal and from which a similarly accurate distance-to-target is computed.
0 Assignments
0 Petitions
Accused Products
Abstract
A combined satellite positioning and electro-optical total station system includes a reference oscillator that provides local oscillator signals for a satellite navigation receiver and a precision frequency source for use by an electronic distance meter. When the satellite navigation receiver is locked onto and tracking orbiting navigation satellites, the highly precise cesium-rubidium clocks in the navigation satellite system can be used as standards to control the reference oscillator in the combined satellite positioning and electro-optical total station system. Baseline measurements made by the electronic distance meter are therefore not subject to mis-calibrations and drift as long as the satellite navigation receiver is locked onto and tracking the orbiting navigation satellites.
36 Citations
18 Claims
-
1. A method of operating an electronic distance meter (EDM) subsystem of a total station, comprising the steps of:
-
substantially continuously receiving from at least one orbiting GPS satellite radio signals with timing information controlled by an atomic clock on board said satellite;
constantly providing a global positioning system (GPS) receiver with a navigation computer for maintaining tracking of said radio signals and for deriving precise timing information from said radio signals;
persistently providing a local reference oscillator with a timing signal based on said derived precise time information;
permanently providing the EDM subsystem with a signal from said oscillator wherein said EDM subsystem sends an outbound laser signal to a distant target and receives an inbound signal reflected by said target;
measuring a difference between said out-bound signal and said resulting in-bound signal reflected from said distant surveyor target to determine the line-of-sight distance to said target;
wherein, the step of measuring provides a signal time-of-flight measurement with an accuracy derived from said precise timing information in said timing signal and from which a similarly accurate distance-to-target is computed. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 18)
said EDM subsystem includes a transmitter for sending said out-bound signal through a telescope to said distant target and a receiver for receiving said in-bound signal through said telescope.
-
-
4. The method of claim 3 wherein:
the step of measuring includes use of a phase measurement device connected to said reference oscillator, said transmitter and said receiver, wherein said phase measurement device provides said time measurement using said reference time base signal.
-
5. The method of claim 1 wherein:
said global positioning system receiver is remotely located to said EDM subsystem, and including the step of, communicating via a radio link between said receiver and said EDM subsystem to drive said EDM system with a signal from said oscillator.
-
6. The method of claim 4 wherein:
said phase measurement device conducts pulse time-of-flight to determine the line-of-sight distance to said target.
-
7. The method of claim 4 wherein:
said phase measurement device conducts carrier phase measurements to determine the line-of-sight distance to said target.
-
8. The method of claim 4 wherein:
the step of measuring the time difference includes observations of a plurality of phase differences observed by said EDM subsystem at a plurality of out-bound and in-bound signals.
-
9. The method of claim 4 further including:
-
mounting said telescope to an angle measurement instrument connected to a servo actuator;
computing in said computer a space vector to target signal;
commanding said servo actuator to direct said telescope towards said target; and
locking in said telescope onto said target.
-
-
10. The method of claim 9 further including:
-
computing a target location seed representing a current position estimate of said telescope;
outputting said target location seed as a position estimate to determine an altitude and azimuth vector to said target;
creating a space vector to target signal from said position estimate;
commanding said servo actuator by said vector to target signal.
-
-
11. The method of claim 1 further including:
-
providing a 1.00 Hz signal from said GPS receiver with timing characteristics derived from said atomic clock; and
stabilizing said local reference oscillator by comparing zero crossings of signals of said local reference oscillator with zero crossings of said 1.00 Hz signal.
-
-
12. The method of claim 1 further including:
-
providing a first 1.00 Hz signal from said GPS receiver with timing characteristics derived from said atomic clock;
reducing the signal frequency of said local reference oscillator to a second 1.00 Hz signal;
phase comparing said first and second 1.00 Hz signals to provide an error signal;
providing the error signal to a phase control port in said local reference oscillator; and
synchronizing said reference oscillator to said 1.00 Hz signal from said GPS receiver.
-
-
18. The method of claim 1 further including the step of:
computing in said navigation computer a current three-dimensional position of the EDM subsystem.
-
13. A method of operating an electronic distance meter (EDM) subsystem of a total station, comprising the steps of:
-
substantially continuously receiving from a time-standard broadcast transmitter source a timing reference signal from which a first comparison signal is derived;
operating a local reference oscillator at a particular frequency of operation;
continuously receiving a first signal from said local reference oscillator and reducing said first signal to a second comparison signal;
constantly phase comparing said first comparison signal with said second comparison signal to provide an error signal;
persistently processing said error signal to create a control signal to provide to said local reference oscillator to obtain phase synchronization of said local reference oscillator with said time-standard broadcast transmitter timing reference signal; and
continuously providing the EDM system with a synchronized reference signal from said local reference oscillator. - View Dependent Claims (14, 15, 16, 17)
said EDM subsystem further provides an out-bound signal directed towards a distance target, and receives an in-bound signal reflected by said target;
measuring a difference between said out-bound signal and said resulting in-bound signal reflected from said distant target to determine the line-of-sight distance to said target; and
wherein the step of measuring provides a signal time-of-flight measurement with an accuracy derived from said time standard broadcast transmitter and from which a similarly accurate distance-to-target estimate is computed.
-
-
15. The method of claim 13 wherein:
said time-standard broadcast transmitter source includes a receiver tuned to receive and synchronized to time data broadcast from NIST via short-wave radio.
-
16. The method of claim 13 wherein:
said time-standard broadcast transmitter source includes a receiver to receive alternate timing signals and to synchronize said time-standard broadcast transmitter to said alternate timing signals, wherein said alternate timing signals are provided from a second time reference station drawn from the group of WWV in Fort Collins, Colo. or WWVH in Hawaii.
-
17. The method of claim 13 wherein:
said time-standard broadcast transmitter includes an orbiting GPS satellite.
Specification