Inertial sensor arrangement

• US 4,823,626 A
• Filed: 06/26/1987
• Issued: 04/25/1989
• Est. Priority Date: 06/30/1986
• Status: Expired due to Term

• Current Assignee: Bodenseewerk Gerätetechnik Gmbh
• Original Assignee: Bodenseewerk Gerätetechnik Gmbh
• Inventors: Fessel, Reinhard, Jansen, Dirk, Hartmann, Ulrich
• Primary Examiner(s): Bonck, Rodney H.
• Application Number:
  US07/067,095
• Time in Patent Office: 669 Days
• Field of Search: 74/5.34, 74/5.46, 74/5.47, 74/5.6 D, 74/5.6 E, 364/453
• US Class Current: 74/5.34
• CPC Class Codes: G01C 19/02 Rotary gyroscopes
• CPC Class Codes: G01C 19/30 Erection devices, i.e. devices for restoring rotor axis to a desired position for instrument indicating the vertical G01C19/46
• CPC Class Codes: G01C 21/183 Compensation of inertial measurements, e.g. for temperature effects
• CPC Class Codes: Y10T 74/1221 Multiple gyroscopes
• CPC Class Codes: Y10T 74/125 by magnetic field
• CPC Class Codes: Y10T 74/1279 Electrical and magnetic

Abstract

An inertial sensor arrangement comprises two electrically restrained gyros with three mutually orthogonal input axes. After A/D-conversion pick-off signals are supplied to a digital computer which forms part of the restraining loop of the gyros and provides digital output signals. The output signals are applied to a D/A-converter which supplies corresponding currents to the torquer of the gyros. Thereby integrating quantization errors are avoided. The cross-coupling behavior and gyro errors can be compensated in the computer. The inertial sensor arrangement can be measured as an entirety. The gyro parameters measured thereby are memorized in an EEPROM and are taken into account in the computer.

Claims

1. Inertial sensor arrangement, comprising

(a) at least one gyro with a spin axis,

(b) a pick-off provided on the gyro and responding to rotational movement about an input axis perpendicular to the spin axis of the gyro and generating a pick-off signal,

(c) a torquer arranged on the gyro to exert a torque on the gyro about an axis perpendicular to the spin axis and to the input axis,

(d) signal processing means, to which the pick-up signal is supplied, said signal processing means being arranged to generate a restraining signal applied to the torquer,

(e) means for generating a digital output signal indicative of the restraining signal, wherein

(f) the pick-off signal is applied to an analog-to-digital converter for generating a digitized pick-off signal

(g) the signal processing means comprise a digital computer which provides said output signal as a digital signal for further processing indicative of angular rate about said input axis, and

(h) the ditigal output signal is applied to a digital-to-analog converter which provides an analog signal as restraining signal which is applied to the torquer.

2. Inertial sensor arrangement as set forth in claim 1, wherein

(a) said gyro forms part of a gyro arrangement with three pick-offs, the pick-offs responding to rotational movements about three mutually orthogonal axes and providing three pick-off signals, and

(b) the pick-off signals are consecutively digitized by a multiplexer and are applied to the computer.

3. Inertial sensor arrangement as set forth in claim 2, including accelerometer means which respond to accelerations in the direction of three mutually orthogonal sensitive axes.

4. Inertial sensor arrangement as set forth in claim 2, wherein the computer is programmed to compensate, according to a gyro error model, the influence of a rotational acceleration about an axis on the measurement of the rotational movement.

5. Inertial sensor arrangement as set forth in claim 3, wherein the computer is programmed to compensate the influence of the linear acceleration on the measurement of the angular rate in accordance with a gyro error model.

6. Inertial sensor arrangement as set forth in claim 1, characterized in that the computer comprises a gyro parameter memory arranged to memorize fixed gyro parameters which are determined by a test of the whole inertial sensor arrangement, these gyro parameters being taken into account in the computer, when the output signal is formed.

7. Inertial sensor arrangement as set forth in claim 1, wherein

(a) at least one temperature sensor is provided

(b) the signals from the temperature sensor are digitized and applied to the computer and

(c) the computer is arranged to compensate the temperature influence on the measurement of the angular rate in accordance with a gyro error model.

8. Inertial sensor arrangement as set forth in claim 1, wherein the computer is combined with the inertial sensors to form a modular unit.

9. Inertial sensor arrangement as set forth in claim 1, wherein the angular-to-digital converter comprises a precision current source which provides a current for the torquer.

10. Inertial sensor arrangement as set forth in claim 1, wherein the gyro is a dynamically tuned gyro.