Feedback system for controlling lock-in in spring suspended ring laser gyroscope

Claim 2

In combination with a spring suspended ring laser gyroscope for providing a gyroscope readout which is proportional to angular input, the gyroscope being suspended by springs from a support; a torquer for dithering the gyroscope relative to the support in response to a control signal; means for measuring the optical phase angle of the gyroscope and providing a signal proportional thereto; means for measuring the movement of the gyroscope relative to the support and providing a signal proportional to dither angle and a signal proportional to dither angular velocity; a feedback unit for generating a control signal which is a function of the optical phase angle signal, the dither angle signal, and the dither angular velocity signal.

Claim 3

The apparatus of claim 1 in which the control signal includes a component which is proportional to dither angular velocity for offsetting system losses due to damping and a piecewise-constant component which is a function of the phase angle of the optical readout for adjusting the phase of the effective dither angular velocity relative to the optical phase angle.

Claim 4

The apparatus of claim 2 in which the piecewise-constant component is generated once for an integral number of cycles and held constant for a time interval equal to that of the integral number of cycles.

Claim 5

The apparatus of claim 2 in which the piecewise-constant is generated once each cycle and held constant.

Claim 6

Apparatus in accordance with claim 4 in which the piecewise-constant control signal component is generated in accordance with the formula ##EQU15## where U n is the value of the piecewise-constant component of torque throughout the nth dither cycle J is the inertia of the sensitive element block Ω is the resonant frequency of the suspension G is the gyro scale factor K is the drive system (torquer) scale factor ψ n is an estimate of the optical pulse angle a In is an estimate of the input rate f 1 is an empirically determined function of the arguments a L , a n , a I f 2 is an empirically determined function of the arguments a L , a n , a I a L is the normalized lock-in rate a n is the normalized dither amplitude k is an integer chosen to keep the quantity within the brackets between -π and π.

Claim 7

An apparatus in accordance with claim 4 in which the feedback unit includes: means for converting the gyro readout angle into a digital value proportional to phase, means including a microprocessor for computing the piecewise-constant component from the digital value once each dither cycle and for converting the digital output of the microprocessor into an analog control signal, and means responsive to the dither angle for initiating computation by the microprocessor once each dither cycle.

Claim 8

An apparatus in accordance with claim 4 in which the gyro readout angle is in the form of fringe detector signals proportional to the sine and cosine of the phase of the angle and the feedback unit includes: means including a microprocessor for computing the piecewise-constant component from the fringe detector signals, for converting the computed signal to analog form, and for holding the computed signal constant, and means responsive to the dither angle for initiating computation in the microprocessor once each dither cycle.

Claim 9

An apparatus in accordance with claim 4 in which the feedback unit includes: means for sampling the gyro readout and for providing a signal proportional to readout angle once each dither cycle, a linear analog circuit responsive to the output of the gyro sampling means for generating the piecewise-constant component, and means for sampling the output of the linear analog circuit once each dither cycle and holding that value constant.

Claim 10

The apparatus of claim 8 in which the analog circuit has the transfer function ##EQU16## in which α 1 , α 2 , β 1 and β 2 are constants.

Claim 13

The method of claim 10 in which the level is established once each cycle.

Claim 14

The method of claim 10 in which the level is a function of gyroscope readout phase angle.

Claim 15

The method of claim 11 in which the level of constant torque is computed from the equation: ##EQU17## U n is the value of the piecewise-constant component of torque throughout the nth dither cycle J is the inertia of the sensitive element block Ω is the resonant frequency of the suspension G is the gyro scale factor K is the drive system (torquer) scale factor ψ n is an estimate of the optical phase angle a I is an estimate of the input rate f 1 is an empirically determined function of the arguments a L , a n , a In f 2 is an empirically determined function of the arguments a L , a n , a In a L is the normalized lock-in rate a n is the normalized dither amplitude k is an integer chosen to keep the quantity within the brackets between -π and π.

Claim 16

The method of claim 12 including computing the signal for controlling the level of constant torque in a microprocessor having as an input, taken once each dither cycle, a signal proportional to the phase of the gyroscope readout angle.

Claim 17

The method of claim 12 including computing a signal for controlling the level of constant torque in an analog computer having as an input, taken one each dither cycle, a signal proportional to the phase of the gyroscope readout angle.

Claim 18

The method of claim 15 in which the analog computer has the transfer function ##EQU18## in which α 1 , α 2 , β 1 and β 2 are constants.