Single gyro northfinder

• US 5,369,889 A
• Filed: 07/07/1986
• Issued: 12/06/1994
• Est. Priority Date: 07/07/1986
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Callaghan, Timothy J., Egli, Werner H.
• Primary Examiner(s): Buczinski, Stephen C.
• Application Number:
  US06/882,865
• Time in Patent Office: 3,074 Days
• Field of Search: 33/318, 33/319, 33/320, 33/321, 33/324, 33/322, 33/337, 33/326, 33/328, 73/178 B, 364/434, 364/559
• US Class Current: 33/321
• CPC Class Codes: G01C 19/38 with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation

Abstract

Disclosed is a northfinding apparatus having a single rotation rate sensor secured to a platform. The output of the rotation rate sensor is corrected for tilt and tilt rate of the platform. Measurements of the tilt and tilt rate and the rotation rate are combined to provide an azimuth angle of the platform relative to north.

Claims

1. A northfinding apparatus comprising:

a platform having a sensor component mounting surface, and associated with said platform is a fixed orthogonal coordinate system defined by X, Y, and Z reference axes, and said Z axis being aligned substantially with vertical relative to the earth'"'"'s surface;

angular rate sensing means secured to said platform, said angular rate sensing means having an input axis aligned substantially with said X axis for providing an output signal R representative of the rotation rate sensed about said input axis;

tilt indicating means, secured to said platform, for providing an output signal representative of the angle of tilt T_x of said platform from true horizontal relative to the center of the earth and about said Y-axis;

tilt rate indicating means, secured to said platform, for providing an output signal S representative of the rate of tilt of said platform about said X-axis;

means for computing the azimuth angle AZ of said platform representative of the angle between said X-axis and the direction of true north as a function of said output signals representative of tilt angle T_x, tilt rate S, and angular rotation rate R, and the earth'"'"'s latitude at which said platform is positioned, and the earth'"'"'s rotation rate.

2. The apparatus of claim 1 wherein said angular rate sensing means is a ring laser angular rate sensor.

3. The apparatus of claim 1 wherein said tilt indicating means comprises a first accelerometer, and said tilt rate indicating means comprises a second accelerometer, and including means for time differentiating said second accelerometer.

4. The apparatus of claim 1 wherein:

said angular rate sensor comprises a ring laser angular rate sensor;

said tilt indicating means comprises a first accelerometer; and

said tilt rate indicating means comprises a second accelerometer and means for taking the time differentiation of the output of said second accelerometer.

5. The apparatus of claim 1 further comprising:

means for rotating said platform between two positions 180 degrees apart;

said computing means including means for computing said azimuth angle AZ for both positions of said platform, and combining said azimuth angle values for said two positions in accordance with a selected function to lessen any bias in said angular rate sensing means output signal.