Method for the autonomous calibration of an inertial rig used in static mode

Patent metadata

Field	Value
Publication number	US-9534926-B2
Application number	US-201414895478-A
Country	US
Kind code	B2
Filing date	Jun 2, 2014
Priority date	Jun 3, 2013
Publication date	Jan 3, 2017
Grant date	Jan 3, 2017

Abstract

The invention relates to a method for the autocalibration of an inertial rig comprising an inertial core defining a sensor reference frame, implemented in the course of at least two missions (M n , M n+1 ) each comprising the determination, on the basis of measurements of gyroscopes, of the orientation of the rig in a reference frame comprising the north axis (N) and the vertical axis (Up), the method comprising the implementation:—in the course of a mission (M n ), of an estimation ( 200 ) of drift errors of the gyroscopes for the orientation of the rig at least with respect to the north axis (dgyrN); and—in the course of a following mission (M n+1 ), of a calculation ( 400 ) of corrections of drift errors (DX n ) of the sensor reference frame (X,Y,Z), on the basis of the estimated drift errors; and—of a calculation ( 600 ) of drift errors (X n+1 ), consisting in correcting drift errors (X n ) of the sensor reference frame that were calculated during the previous mission (M n ).

First claim

The invention claimed is:

1. An auto-calibration method of inertial equipment ( 1 ) comprising an inertial core ( 10 ) forming a sensor reference frame, said core comprising at least two gyroscopes,
the method being executed during at least two successive missions (Mn, Mn+1) of the inertial equipment ( 1 ), each mission being a static phase comprising determination, from measurements of the gyroscopes ( 11 ), of the orientation of the equipment ( 1 ) in a geographic reference frame comprising the axis of the North (N) and the axis of the vertical (Up), the relative positions of the sensor reference frame (X,Y,Z) and of the geographic reference frame being different from one mission to the other,
the method being characterized by carrying out:
during a mission (Mn) of the equipment ( 1 ) estimation ( 200 ) of drift errors of the gyroscopes on the orientation of the equipment at least relative to the axis of the North (dgyrN), and
during a following mission (Mn+1) of calculation of drift ( 400 ) error corrections (DXn) of the sensor reference frame (X,Y,Z), from drift errors estimated on the orientation of the equipment, and
calculation of drift (Xn+ 1 ) errors ( 600 ) of the sensor reference frame (X, Y,Z) including correcting by means of said corrections (DXn) of drift errors of the sensor reference frame, the drift errors (Xn) of the sensor reference frame having been calculated during the preceding mission (Mn).

2. The auto-calibration method according to claim 1 , the inertial equipment being an inertial unit ( 1 ), whereof the inertial core ( 10 ) comprises three accelerometers ( 12 ) and three gyroscopes ( 11 ),
wherein the estimation step ( 200 ) of drift errors (dgyrUp,dgyrN) of the gyroscopes further comprises estimation of drift errors of the gyroscopes relative to the axis of the vertical.

3. The auto-calibration method according to claim 1 , wherein the calculation ( 400 ) of drift (DXn) error corrections of the sensor reference frame (X,Y,Z) is performed by means of a Kalman filter.

4. The auto-calibration method according to claim 1 , wherein estimation ( 200 ) of the drift errors of the gyroscopes is performed at a predetermined frequency, and calculation ( 400 ) of the drift error corrections is performed from estimations of averaged drift errors ( 300 ).

5. The auto-calibration method according to claim 1 , reference frame comprising prior to each calculation step ( 600 ) of drift errors of the sensor reference frame, determination ( 500 ) of the standard deviation of drift error corrections (DXn) of the sensor reference frame for each axis of the sensor reference frame, determining that the standard deviation of the correction of drift errors of the corresponding axis is less than a predetermined threshold, and calculation of drift errors ( 600 ) of the sensor reference frame for an axis.

6. The auto-calibration method according to claim 1 , wherein the date of each usage session of the inertial equipment ( 1 ) is stored, the correction calculation of drift errors ( 400 ) of the sensor reference frame taking into account the temporal evolution of the drift errors of the sensor reference frame according to an ageing law linked to the gyroscopes ( 11 ).

7. The auto-calibration method according to claim 1 , wherein determination of the orientation of the inertial equipment in the geographic reference frame from measurements of gyroscopes and estimation ( 200 ) of drift errors of gyroscopes on said orientation are carried out by means of a Kalman filter.

8. A computer program product comprising code instructions for executing the calibration method according to claim 1 when the latter is executed by a computer ( 30 ).

9. Inertial equipment ( 1 ) comprising an inertial core ( 10 ) forming a sensor reference frame (X, Y ,Z), said inertial core ( 10 ) comprising at least two gyroscopes ( 11 ), a memory ( 40 ), and a computer ( 30 ), the inertial equipment ( 1 ) being characterized in that the computer ( 30 ) is configured to execute the method according to claim 1 .

10. The inertial equipment according to claim 9 , said equipment being an inertial unit whereof the inertial core ( 10 ) comprises three accelerometers ( 12 ) and three gyroscopes ( 11 ).

11. A processing system comprising inertial equipment ( 1 ) including an inertial core ( 10 ) forming a sensor reference frame, said core comprising at least two gyroscopes, said system also comprising a memory ( 40 ) and a computer ( 30 ), adapted to communicate remotely with the inertial equipment ( 1 ), the system being characterized in that the computer is configured to execute the method according to claim 1 .

Assignees

• Sagem Defense Securite

Inventors

• Roberfroid David
• Cournou Vincent

Classifications

• G01P21/00

  Testing or calibrating of apparatus or devices covered by the preceding groups · CPC title

• G01C25/005 Primary

  initial alignment, calibration or starting-up of inertial devices · CPC title

• G01C19/38

  with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation · CPC title

• G01C21/165

  combined with non-inertial navigation instruments · CPC title