Analog torque rebalance loop for a tuned rotor gyroscope

• US 5,138,883 A
• Filed: 09/28/1990
• Issued: 08/18/1992
• Est. Priority Date: 09/29/1989
• Status: Expired due to Fees

• Current Assignee: Her Majesty The Queen As Represented By The Minister of National Defence of Her Majesty's Canadian Government
• Original Assignee: Her Majesty The Queen As Represented By The Minister of National Defence of Her Majesty's Canadian Government
• Inventors: Gallop, Lloyd, Vinnins, Michael F., Paquet, Francois
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US07/589,533
• Time in Patent Office: 690 Days
• Field of Search: 73/504, 73/510, 74/5 F, 74/5.4
• US Class Current: 73/504.18
• CPC Class Codes: G01C 19/04 Details
• 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: Y10T 74/1229 Gyroscope control

Abstract

A rebalance loop for controlling a dry tuned rotor gyroscope having a rotor moveable about two orthogonal axes, a first pickoff associated with one of the axes for producing an electrical error signal when a rate is applied to one of the axes, a second pickoff associated with the other of the axes for producing an electrical error signal when a rate is applied to that axis and a pair of torquer coil adapted to receive electrical control signals from the rebalance loop and apply torques to the rotor about the two axes for correcting errors detected by the pickoffs. The rebalance loop comprises a first direct-axis loop which receives an error signal produced by one of the pickoffs and produces a first amplified error signal, a second direct-axis loop which receives an error signal produced by the other of the pickoffs and produces a second amplified error signal, a first cross-axis loop for amplifying the error signal produced by the one of the pickoffs and adapted to produce a first correction signal, a second cross-axis loop for amplifying the error signal produced by the other of the pickoffs and adapted to produce a second correction signal, a first summing junction for adding the first correction signal to the second amplified error signal for producing a first torque correction signal, and a second summing junction for adding the second correction signal to the first amplified error signal for producing a second torque correction signal.

Claims

1. A rebalance loop for a dry tuned rotor gyroscope having a rotor moveable about two orthogonal axes, means associated with one of said axes for producing an electrical error signal when a rate is applied to said one of said axes, means associated with the other of said axes for producing an electrical error signal when a rate is applied to said other of said axes, first means responsive to a first torque control signal for applying a torque to said rotor about one of said axes for restoring said rotor to a null position about said one of said axes and second means responsive to a second torque control signal for applying a torque to said rotor about the other of said axes for restoring said rotor to a null position about said other of said axes and said rebalance loop comprising:

first direct-axis circuit means responsive to one of said error signals for producing a first rate proportional torque signal and delivering said first rate proportional torque signal to said first means;

second direct-axis circuit means responsive to the other of said error signals for producing a second rate proportional torque signal and delivering said second rate proportional torque signal to said second means;

first cross-axis circuit means responsive to said one of said error signals for producing a first acceleration proportional torque signal and delivering said first acceleration proportional torque signal to said second means; and

second cross-axis circuit means responsive to said other of said error signals for producing a second acceleration proportional torque signal and delivering said second acceleration proportional torque signal to said first means.

2. A rebalance loop as defined in claim 1, each said direct-axis circuit means including a nutation low-pass filter means for introducing a phase lag into a filtered input signal and torquer driver means for receiving and amplifying the output of said filter means and said acceleration proportional torque signal and producing said torque control signal.

3. A rebalance loop as defined in claim 2, said torquer driver means including an operational amplifier and an inverting push-pull amplifier for amplifying the output of said operational amplifier, said operational amplifier being adapted to receive, at its inverting input, said output of said filter means and, at its non-inverting input, the signal received at a return line from said means responsive to a first torque control signal and said acceleration proportional torque signal from its associated cross-axis circuit means.

4. A rebalance loop as defined in claim 1, each said cross-axis circuit means including a nutation notch filter and a differentiator for differentiating the output of said nutation notch filter and producing one of said acceleration proportional signals.

5. A rebalance loop as defined in claim 2, each said cross-axis circuit means including a nutation notch filter and a differentiator for differentiating the output of said nutation notch filter and producing one of said acceleration proportional signals.

6. A rebalance loop as defined in claim 1, further including:

a first front-end circuit means associated with said first direct-axis circuit means and said second cross-axis circuit means adapted to receive said one of said error signals and a second front-end circuit means associated with said second direct-axis circuit means and said first cross-axis circuit means adapted to receive said other of said error signals, each said front-end circuit means including an AC amplifier for amplifying one of said error signals, a demodulator for demodulating said error signal, a low pass filter for filtering said demodulated error signal, an integrator for integrating said output of said filter, and a spin notch filter for filtering the output of said integrator and delivering an input signal to its associated direct-axis circuit means and cross-axis circuit means.

7. A rebalance loop as defined in claim 6, said low pass filter being arranged to provide a minimized phase delay at frequencies near the gain crossover frequency where the open loop gain is unity and to provide a predetermined amount of phase lag at the nutation frequency of the gyroscope.

8. A rebalance loop as defined in claim 6, further including a phase splitting transformer for minimizing the DC offset and drift of said demodulator, said transformer having a primary winding connected to the output of said AC amplifier and a secondary connected to said demodulator.

9. A rebalance loop as defined in claim 6, further including means for applying a reference signal to said demodulator.

10. A rebalance loop as defined in claim 9, said reference signal being a sine wave, and said means being adapted to convert said sine wave signal to a square wave, further including means for splitting said square wave and applying two complementary square waves having coincident transitions to said demodulator.

11. A rebalance loop as defined in claim 6, wherein said integrator being adapted to integrate the filtered output of said demodulator from DC to 3 Hz so as to make the steady state stiffness of the system infinite.

12. A rebalance loop as defined in claim 5, said torquer driver means including an operational amplifier and four darlington transistors adapted to receive the output of said operational amplifier.

13. A rebalance loop for a dry tuned rotor gyroscope having a rotor moveable about two orthogonal axes, means associated with one of said axes for producing an electrical error signal when a rate is applied to said one of said axes, means associated with the other of said axes for producing an electrical error signal when a rate is applied to said other of said axes, a first torquer coil responsive to a first torque control signal for applying a torque to said rotor about one of said axes for restoring said rotor to a null position about said one of said axes and a second torquer coil responsive to a second torque control signal for applying a torque to said rotor about the other of said axes for restoring said rotor to a null position about said other of said axes, said rebalance loop comprising;

first front-end circuit means for demodulating one of said error signals, filtering any residual carrier signal and spin noise from said one error signal, introducing a first predetermined amount of phase lag into said one error signal, and integrating said one error signal whereby to produce a first filtered and integrated signal;

second front-end circuit means for demodulating the other of said error signals, filtering any residual carrier signal and spin noise from said other of said error signal, introducing a first predetermined amount of phase lag into said other error signal, and integrating said other error signal whereby to produce a second filtered and integrated signal;

first cross-axis circuit means for filtering from said second filtered and integrated signal a predetermined band of frequencies centered on the nutation frequency of said gyroscope and differentiating sad signal whereby to produce a first acceleration proportional torque signal;

second cross-axis circuit means for filtering from said first filtered and integrated signal a predetermined band of frequencies centered on the nutation frequency of said gyroscope and differentiating said signal whereby to produce a second acceleration proportional torque signal;

first direct-axis circuit means responsive to said first filtered and integrated signal for adding thereto a second predetermined amount of phase lag by a first nutation low-pass filter whereby to produce a first rate proportional torque signal and responsive to said first acceleration proportional torque signal to combine said first rate proportional torque signal and said first acceleration proportional torque signal to produce a first torque control signal and convert said first torque control signal in a first torquer driver to a form capable of driving said first torquer coil;

second direct-axis circuit means responsive to said second filtered and integrated signal for adding thereto a second predetermined amount of phase lag by a second nutation low-pass filter whereby to produce a second rate proportional torque signal and responsive to said second acceleration proportional torque signal to combine said second rate proportional torque signal and said second acceleration proportional torque signal o produce a second torque control signal and convert said second torque control signal in a second torquer driver to a form capable of driving said second torquer coil;

said first torquer driver including an operational amplifier and an inverting push-pull amplifier for amplifying the output of said operational amplifier, said operational amplifier being adapted to received, at its inverting input, an output of said first nutation low-pass filter and, at its non-inverting input, the signal received at a return line from an output terminal of said first torquer coil to which output a signal from the second cross-axis circuit means is applied; and

said second torquer driver including a further operational amplifier and a further inverting push-pull amplifier for amplifying the output of said further operational amplifier, said further operation amplifier being adapted to receive, at its inverting input, an output of said second nutation low-pass filter and, at its noninverting input, the signal received at a return line from an output terminal of said second torquer coil, to which output a signal from the first cross-axis circuit means is applied.

14. A rebalance loop as defined in claim 13, further including a first precision resistor connected between said output terminal of said first torquer coil and ground and wherein said signal thereat is a voltage and a second precision resistor connected between said output terminal of said second torquer coil and ground and wherein said signal thereat is a voltage.