Device for calibrating ultra-sensitive accelerometers

• US 4,869,092 A
• Filed: 12/18/1987
• Issued: 09/26/1989
• Est. Priority Date: 12/18/1986
• Status: Expired due to Fees

• Current Assignee: Office National D'Etudes et de Recherches Aerospatiales
• Original Assignee: Office National D'Etudes et de Recherches Aerospatiales
• Inventors: Bernard, Alain, Touboul, Pierre
• Primary Examiner(s): Noland, Tom
• Application Number:
  US07/135,091
• Time in Patent Office: 648 Days
• Field of Search: 73/1 D, 73/1 R, 73/1 E, 73/510, 73/511, 73/512, 73/2, 73/517 R, 73/517 AV, 73/517 B, 73/517 A
• US Class Current: 73/1.38
• CPC Class Codes: G01P 21/00 Testing or calibrating of apparatus or devices covered by the preceding groups

Abstract

Measuring instruments, such as ultra-sensitive accelerometers, are attached to a support inlcuding three pairs of electrodynamic or piezoelectric actuators. Each actuator pair is associated with one respective common axis of a reference trirectangular system. An electronic speed and phase slaver chains the actuators to induce translational and rotational accelerations in the support. Electrical signals delivered from the instruments to be calibrated are analyzed by synchronous demodulations and processed to determine sensitivity, orientation and position of the instruments in relation to the reference axes. The instrument support can be carried on-board a satellite.

Claims

1. A device for calibrating acceleration-sensitive measuring instruments, said instruments being attached to a support and delivering electrical signals in response to acceleration actions, said device comprising three parts of actuators respectively associated with three reference axes forming a trirectangular trihedral for applying accelerations to said instrument support along said three reference axes whereby each of said actuator pairs induces periodic translational and rotational accelerations.

2. The device claimed in claim 1, wherein said actuators of each of said pairs operate with rotative motion and a dynamic unbalanced weight and are laid out symmetrically on either side of a point where said reference axes intersect.

3. The device claimed in claim 2, wherein said actuators are electric motors attached to said instrument support, each pair of said actuators having an axis of rotation coaxial with the respective reference axis, each of said actuators comprising a rotative unbalanced weight and a phase detector for the rotation of said unbalance weight.

4. A device as claimed in claim 3 comprising means of controlling said electric motors with periodic voltages, whereby said actuators induce sinusoidal accelerations, said electrical signals delivered from said instruments to be calibrated being analyzed by synchronous demodulating means.

5. The device claimed in claim 1, wherein said actuators operate with linear motion and are laid out on the same side of a point where said reference axes intersect.

6. The device claimed in claim 5, wherein said actuators are placed between said instrument support and a rigid frame, each of said actuator parts being symmetrically laid out in relation to the respective reference axis and acting in a plane containing a respective face of said trihedral.

7. The device claimed in claim 6 wherein said actuators are electrodynamic.

8. The device claimed in claim 6 wherein said actuators are piezoelectric.

9. A device as claimed in claim 6 comprising three parts of position detectors for detecting positions of said instrument support with respect to said reference axes, said three detector pairs being respectively close to trihedral faces parallel to said faces that with which said three actuators pairs are respectively coplanar, means for generating periodic signals, and instrument support position slaving means receiving signals from said position detectors and said periodic signals for supplying electric control signals to said actuators whereby said actuators induce sinusoidal accelerations, said electric signals delivered by said instruments to be calibrated being analyzed by synchronous demodulating means.

10. The device claimed in claim 9, wherein said actuators are electrodynamic and are placed between said instrument support and a rigid frame, said device being carried on-board a compensated-drag satellite, and said support comprising a drag compensation detector with a test weight.

11. A device as claimed in claim 10 wherein said actuators are controlled to induce sinusoidal translational accelerations and are included in a support position slaving chain receiving test weight position detection signals, the displacement of said test weight being controlled by voltages delivered by a voltage generator.

12. The device claimed in claim 11, wherein said test weight in said drag compensation detector is spherical, free and floating in a cage carrying spherical cap electrodes, said electrodes being isolated from said cage and aligned in pairs along three orthogonal axes, and wherein said electrodes for each of said axes constitute both electrodes of a test weight position capacitive detector and electrostatic force application electrodes for changes of displacement of said test weight.

13. A calibration method for instruments sensitive to accelerations, said instruments being attached to a support and delivering electrical signals in response to acceleration actions, said method comprising applying periodic translational and rotational accelerations to said instrument support along three reference axes forming a trirectangular trihedral, and collecting said electrical signals delivered from said instruments to be calibrated thereby deducing the characteristics of said instruments, said periodic translational and rotational accelerations being induced by three pairs of actuators respectively associated with said three reference axes.

14. The calibration method claimed in claim 13, wherein said three actuator pairs induce three sinusoidal accelerations having distinct frequencies for said reference axes, respectively, said electric signals delivered from said instruments being analyzed by synchronous demodulations and processed to determine sensitivity, orientation and position of said instruments in relation to said reference axes.

15. A calibration method for instruments sensitive to accelerations, said instruments being attached to a support and delivering electrical signals responsive to acceleration actions, said support being carried on-board a compensated-drag satellite, said method comprising applying periodic translational accelerations to said instrument support along three reference axes forming a trirectangular trihedral, in) collecting said electrical signal delivered from said instruments to be calibrated thereby deducing characteristics of said instruments, said periodic translational accelerations being induced by three pairs of electrodynamic actuators respectively associated with said three reference axes and being respectively included in three loops for position-slaving said instrument support in relation to a test weight, said test weight being included in a drag compensation detector of said satellite, said drag compensation detector being capacitive and having three pairs of electrodes respectively associated with said three reference axes, applying two oppositely phased detection voltages to said two electrodes of each of said electrode pairs respectively, during instrument calibration phases applying calibration acceleration generation voltages to said two electrodes associated with a predetermined one of said reference axes and other voltages having half amplitudes and opposite phases to those of said calibration acceleration generation voltages, said electrical signals delivered from said measuring instruments to be calibrated being analyzed by synchronous demodulations and processed to determine sensitivity, orientation and position of said instruments in relation to said reference axes.