Centimeter accurate global positioning system receiver for on-the-fly real-time kinematic measurement and control

• US 5,519,620 A
• Filed: 02/18/1994
• Issued: 05/21/1996
• Est. Priority Date: 02/18/1994
• Status: Expired due to Term

• Current Assignee: Trimble Navigation Limited (Trimble Inc.)
• Original Assignee: Trimble Navigation Limited (Trimble Inc.)
• Inventors: Nichols, Mark E., Talbot, Nicholas C., Allison, Michael T.
• Primary Examiner(s): ZANELLI, MICHAEL J
• Application Number:
  US08/199,387
• Time in Patent Office: 823 Days
• Field of Search: 364/449, 364/424.01, 364/424.02, 342/357, 342/457, 342/442, 342/444, 348/118, 348/119, 348/135, 348/142, 348/148, 318/587
• US Class Current: 701/214
• CPC Class Codes: G01S 19/04 providing carrier phase data
• CPC Class Codes: G01S 19/32 Multimode operation in a single same satellite system, e.g. GPS L1/L2
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method

Abstract

A system embodiment of the present invention comprises a fixed and a roving pair of four-observable GPS receivers and a communication link between them for double differencing code and carrier measurements. Carrier phase integer ambiguities are resolved efficiently by searching the simultaneous narrow-lane intersections of both the L1 and L2 wave fronts propagated by the GPS satellites being tracked. External constraint information, such as elevation, is additionally used to speed up integer ambiguity resolution. Data between the reference station and the rover is communicated in compressed form at a regular interval, e.g., once a second at each epoch, and demi-measurements of carrier phase are obtained more frequently, e.g., ten times a second, and used to propagate solutions between epochs.

Claims

1. An on-the-fly real-time kinematic (OTF-RTK) system for use with the global positioning system (GPS), comprising:

a reference station (12,

     126) including a GPS satellite navigation receiver and measurement means (70, 72, 74,

     76) connected to output (19,

     128) single carrier frequency code and phase measurements from a fixed location;

a rover unit (14,

     130) including a GPS satellite navigation receiver and measurement means (90, 92, 94,

     96) connected to output (132) single carrier frequency code and phase measurements from a movable vehicle and including an output for position determinations;

double-differencing means (98) connected to receive phase and code measurement information transmitted from the reference station and rover unit and then difference said measurement information to subtract out satellite-common and receiver-common clock errors, wherein substantially unbiased phase and code measurement information is output;

integer ambiguity resolution means (106) connected to the double-differencing means and including integer search means for searching carrier frequency phase and code measurements, wherein a unique solution for whole-cycle carrier phase ambiguity is provided at an output to computer navigation means for positioning determining with centimeter-level accuracy and on-the-fly initialization;

a navigation computer (108) connected to receive said unbiased phase and code measurement information and to provide an output of near-continuous position estimates of the rover unit; and

robotic control means (134) connected to receive said near-continuous position estimates from the navigation computer in the rover unit for servo-controlling a remote-controlled vehicle according to a plurality of comparisons made between said near-continuous position estimates and a predetermined construction model of ideal positions for said remote-controlled vehicle.

2. An on-the-fly real-time kinematic (OTF-RTK) system, comprising:

a reference station (12,

     126) including a satellite navigation receiver and measurement means connected to output carrier frequency code and phase measurements from a fixed location;

a rover unit (14,

     130) including a satellite navigation receiver and measurement means connected to output carrier frequency code and phase measurements from a movable vehicle;

double-differencing means (98) connected to receive phase and code measurement information transmitted from the reference station and rover unit and the difference said measurement information to subtract out satellite-common and receiver-common clock errors, wherein substantially unbiased phase and code measurement information is output;

integer ambiguity resolution means (106) connected to the double-differencing means and including integer search means for simultaneously searching the phase of said carrier frequency phase measurements, wherein a unique solution for whole-cycle carrier phase ambiguity is provided at an output to a navigation computer means for positioning determining with centimeter-level accuracy and on-the-fly initialization; and

a navigation computer (108) connected to receive said unbiased phase and code measurement information and to provide an output of near-continuous position estimates of the rover unit.

3. The system of claim 2, further comprising:

height constraint means (107) connected to the integer ambiguity resolution means for reducing the search space of ambiguous carrier phase integers by introducing at least one of an elevation, separation distance and orientation constraint.

4. The system of claim 2, further comprising:

a radio transmitter (82) connected to the reference station and a radio receiver connected to the rover unit for effecting said connection of the double-differencing means to the reference station and for communicating said first and second carrier frequency code and phase measurements from the reference station to the rover unit;

data compression and decompression means (80,

     102) connected in series with the radio transmitter and the radio receiver for lowering the data traffic volume necessary to communicate said first and second carrier frequency code and phase measurements over a radio channel;

time-tag and epoch means (78) connected to said satellite navigation receiver and measurement means in the reference station for time-tagging said first and second carrier frequency code and phase measurements; and

epoch synchronizing means included in the double-differencing means (98) for matching said first and second carrier frequency code and phase measurements in same-epoch pairs for epoch-synchronized double-differencing and providing for a main-measurement update each epoch.

5. The system of claim 2, further comprising:

propagation means (104) connected to the double-differencing means and a demi-epoch timing means for propagating a plurality of demi-epoch position updates from said unbiased phase and code measurement information between said main-measurement updates.

6. The system of claim 2, further comprising:

datum transformation means (110) connected to the navigation computer in the rover unit for outputting centimeter-level accurate position fixes in a local coordinate format from said near-continuous position estimates of the rover unit; and

ellipsoid-to-geoid conversion means (112) connected to the datum transformation means for outputting locally corrected height information from said near-continuous position estimates of the rover unit.

7. The system of claim 2, further comprising:

a remotely-controlled vehicle (122) associated with the rover unit for guidance by a controller in response to said near-continuous position estimates of the rover unit.

8. The system of claim 2, further comprising:

a servo-controlled mechanism (140) proximate to the rover unit;

a computer-based digital model (136) of guidance plan position information for providing guidance plan position information;

controller means (134) including an input from the computer-based digital model and an input (132) for said near-continuous position estimates of the rover unit and an output (138) for a servo control signal connected to the servo-controlled mechanism for guiding the rover unit with the servo-controlled mechanism according to a comparison of said guidance plan position information to said near-continuous position estimates of the rover unit; and

communication means (138) connected between the controller means and the servo-controlled mechanism for said servo control signal.

9. The system of claim 8, further comprising:

a video camera (142) proximate to the servo-controlled mechanism; and

a video monitor (146) remote to the video camera and in communication with the video camera for providing a user with a visual display of an area proximate to the rover unit.