High speed well surveying and land navigation

• US 4,833,787 A
• Filed: 06/11/1987
• Issued: 05/30/1989
• Est. Priority Date: 08/23/1985
• Status: Expired due to Fees

• Current Assignee: Applied Technologies Associates, Inc.
• Original Assignee: Applied Technologies Associates, Inc.
• Inventors: Van Steenwyk, Donald H.
• Primary Examiner(s): Martin, Jr., William D.
• Application Number:
  US07/060,648
• Time in Patent Office: 719 Days
• Field of Search: 33/141.5, 33/333, 33/304, 33/318, 33/313, 33/312, 33/324, 33/302
• US Class Current: 33/302
• CPC Class Codes: E21B 47/022 of the borehole, e.g. using geomagnetism
• CPC Class Codes: G01C 21/16 by integrating acceleration or speed, i.e. inertial navigation

Abstract

A land vehicle navigation apparatus incorporates an inertial angular rate sensor on the vehicle and having a sensitive axis, and an inertial acceleration or tilt sensor having at least two sensitive axes; the latter two sensitive axes are typically located at the vehicle in a plane parallel to the Earth'"'"'s surface; and a rotary drive is operatively connected to the sensors to rotate them about an axis extending generally at the vehicle in a plane parallel to the Earth'"'"'s surface; and, circuitry is operatively connected with the sensors to determine three vehicle orientation angles, roll, pitch, and azimuth, with respect to an Earth-fixed coordinate set at a first location, and also to determine the three vehicle orientation angles as the land vehicle travels over the Earth surface; and changes to the azimuth angle during travel are determined by integration of the output of the rate sensor; also, the sensor, drive and circuitry are typically carried by the vehicle.

Claims

1. In a land vehicle navigation apparatus, the combination comprising

(a) intertial angular rate sensor means having a sensitive axis,

(b) inertial acceleration or tilt sensor means having at least two sensitive axes, said sensitive axes being nominally orthogonal to said inertial angular rate sensor'"'"'s sensitive axis,

(c) means to accept from an external source an initial value of the vehicle'"'"'s azimuthal orientation angle with respect to an Earth-fixed coordinate set, and

(d) circuitry operatively connected with said (a) and (b) sensor means and said (c) input acceptance means to determine three vehicle orientation angle, roll, pitch, and azimuth, with respect to an Earth-fixed coordinate set as the land vehicle travels over the Earth surface, and wherein changes to said azimuth angle during travel are determined by integration of the output of said (a) sensor means,

(e) and a land vehicle supporting said (a) and (b) means, and having support means on which the vehicle travels over the Earth'"'"'s surface.

2. The apparatus of claim 1 including a means to accept an external input that is a measure of the distance-of-travel of the vehicle over the Earth surface, whereby said vehicle orientation angles may be used with said distance-of-travel to comput vehicle position changes during vehicle travel.

3. The apparatus of claim 2 including means enabling use of said external input measure of vehicle distance-of-travel to compute vehicle linear and centripetal accelerations to correct the roll and pitch vehicle orientation angles computed from said (b) sensor means.

4. In a land vehicle navigation apparatus, the combination with the vehicle comprising

(a) inertial angular rate sensor means having a sensitive axis,

(b) inertial acceleration or tilt sensor means having at least two sensitive axes, said sensitive axes being arranged to be nominally located at the vehicle in a plane parallel to the Earth'"'"'s surface,

(c) a rotary drive operatively connected to said (a) means to rotate said (a) means about an axis extending generally at the vehicle in a plane parallel to the Earth'"'"'s surface,

(d) circuitry operatively connected with said (a) and (b) sensor means to determine three vehicle orientation angles, roll, pitch, and azimuth, with respect to an Earth-fixed coordinate set at a first location, and to also determine said three vehicle orientation angles as the land vehicle travels over the Earth surface wherein changes to said azimuth angle during travel are determined by integration of the output of said (a) sensor means,

(e) said (a) and (b) means and said (c) drive being carried by the vehicle, having support means on which the vehicle travels over the earth'"'"'s surface.

5. The apparatus of claim 4 including a means to accept an external input that is a measure of the distance-of-travel of the vehicle over the Earth surface for enabling use of said vehicle orientation angles with said distance-of-travel to compute vehicle position changes during travel.

6. The apparatus of claim 5 including means for enabling use of said external input measure of vehicle distance-of-travel to compute vehicle linear and centripetal accelerations to correct the roll and pitch vehicle orientation angles computed from said (b) sensor means.

7. In a land vehicle navigation apparatus, the combination for use with the vehicle comprising:

(a) inertial angular rate sensor means having a sensitive axis,

(b) inertial acceleration or tilt sensor means having at least two sensitive axes, said sensitive axes being arranged to be nominally located at the vehicle in a plane parallel to the Earth'"'"'s surface,

(c) a rotary drive operatively connected to said (a) and (b) means to rotate said (a) and (b) means about an axis extending generally at the vehicle in a plane parallel to the Earth'"'"'s surface,

(d) circuitry operatively connected with said (a) and (b) sensor means to determine three vehicle orientation angles, roll, pitch, and azimuth, with respect to an Earth-fixed coordinate set at a first location, and to also determine said three vehicle orientation angles as the land vehicle travels over the Earth surface wherein changes to said azimuth angle during travel are determined by integration of the output of said (a) sensor means,

(e) said (a) and (b) means, and said (c) drive and (d) circuitry being carried by the vehicle, which has support means on which the vehicle travels over the earth'"'"'s surface.

8. The apparatus of claim 7 including means to accept an external input that is a measure of the distance-of-travel of the vehicle over the Earth surface for enabling use of said vehicle orientation angles with said distance-of-travel to compute vehicle position changes during travel.

9. The apparatus of claim 8 including error correcting means for enabling use of said external input measure of vehicle distance-of-travel to compute vehicle linear and centripetal accelerations to correct the roll and pitch vehicle orientation angles computed from said (b) sensor means.

12. In method of operating apparatus as defined in claim 7, the steps that include:

(i) operating said device to rotate the input axis of sensitivity of the rate sensor means about an axis extending in the direction of vehicle travel to two or more discrete positions,

(ii) and processing the output of said rate sensor means to derive initial vehicle azimuth.

13. The method of claim 12 including:

(iii) positioning said input axis of sensitivity of the rate sensor means to be parallel to the vehicle Z axis that is characterized as perpendicular to the vehicle direction of travel and upright relative to the vehicle.

10. In a land vehicle navigation apparatus, the combination comprising

(a) inertial angular rate sensor means having a sensitive axis,

(b) inertial acceleration or tilt sensor means having at least two sensitive axes, said sensitive axes being nominally orthogonal to said inertial angular rate sensor'"'"'s sensitive axis,

(c) means to accept from an external source an initial value of the vehicle'"'"'s azimuthal orientation angle with respect to an Earth-fixed coordinate set, and

(d) circuitry operatively connected with said (a) and (b) sensor means and said (c) input acceptance means to determine three vehicle orientation angles, roll, pitch, and azimuth, with respect to an Earth-fixed coordinate set as the land vehicle travels over the Earth surface, and wherein changes to said azimuth angle during travel are determined by integration of the output of said (a) sensor means,

(e) and a land vehicle supporting said (a) and (b) means, and having support means on which the vehicle travels over the Earth'"'"'s surface,

(f) means to accept an external input that is a measure of the distance-of-travel of the vehicle over the Earth surface for enabling use of said vehicle orientation angles with said distance-of-travel to compute vehicle position changes during travel,

(g) error correcting means for enabling use of said external input measure of vehicle distance-of-travel to compute vehicle linear and centripetal accelerations to correct the roll and pitch vehicle orientation angles computed from said b) sensor means.

(b) said error correcting means including a first integrator to integrate output provided by said angular rate sensor means along the vehicle direction of travel, and a second integrator to integrate output of the first integrator, and subtractor means to subtract the output of the second integrator from said external input to provide an output fed back to the second integrator with selected gains, whereby linear acceleration is corrected.

11. The apparatus of claim 10 wherein said error correcting means includes a multiplier, having one input connected to receive output from the first integrator, and another input connected to receive output from said inertial acceleration or tilt sensor means, and a subtractor connected to the output of the multiplier and to the output of the inertial angular rate sensor means, as directionally related to the vehicle direction of movement, to provide an output correction for centripetal acceleration.

14. In a land navigation apparatus, the combination for use with the vehicle comprising

(a) inertial angular rate sensor means having a sensitive axis,

(b) inertial acceleration or tilt sensor mean shaving at least two sensitive axes, said sensitive axes being arranged to be nominally located at the vehicle in a plane parallel to the Earth'"'"'s surface,

(c) a rotary drive operatively connected to said (a) and (b) means to rotate said (a) and (b) means about an axis extending generally at the vehicle in a plane parallel to the Earth'"'"'s surface,

(d) circuitry operatively connected with said (a) and (b) sensor means to determine three vehicle orientation angles, roll, pitch, and azimuth, with respect to an Earth-fixed coordinate set at a first location, and to also determine said three vehicle orientation angles as the land vehicle travels over the Earth surface wherein changes to said azimuth angle during travel are determined by integration of the output of said (a) sensor means,

(e) said (a) and (b) means, and said (c) drive and (d) circuitry being carried by the vehicle which has support means on which the vehicle travels over the earth'"'"'s surface,

(f) and wherein an erroneous indicated rate-of-change of the vehicle azimuth angle is at times produced by said integration, and including apparatus to detect that the vehicle is stopped, to measure said erroneous indicated rate-of-change of the vehicle azimuth angle, and to compute corrections to be applied in subsequent operations to reduce said erroneous rate-of-change of azimuth angle.

15. In the method of operating land navigation apparatus incorporating the apparatus of claim 14, the step that includes:

(i) stopping the vehicle periodically for a fixed known time to permit the apparatus to determine any erroneous rate-of-change of vehicle azimuth and to develop corrections to such erroneous rate, for subsequent use.