Nutation damper for two-axis gyroscope

Claim 2

In a two-axis gyroscope having mutually perpendicular first and second reference axes, a rotor with a spin axis, a first pickoff which produces a first pickoff signal whose magnitude is proportional to the angle the rotor spin axis makes with respect to the first reference axis, a second pickoff which produces a second pickoff signal whose magnitude is proportional to the angle the rotor spin axis makes with respect to the second reference axis, a first torquer which produces angular accelerations of the rotor about the first reference axis, a second torquer which produces angular accelerations of the rotor about the second reference axis, and control means for producing first and second torquer control signals from the first and second pickoff signals which control the amount of angular accelerations produced by the first and second torquers, respectively, the improvement comprising: the control means including damping means for stably damping variations in the magnitudes of the first and second pickoff signals occurring at the nutation frequency which damping means use the first and second pickoff signals to produce torquer control signals which cause substantial angular accelerations only when the first and second pickoff signal variations occur at the nutation frequency and which cause no angular accelerations when there are no variations in the magnitudes of the first and second pickoff signals at the nutation frequency; and blocking capacitors disposed between said damping means and the first and second torquers.

Claim 3

The invention according to claim 1 and further includes means for adjusting amount of damping produced by the damping means.

Claim 4

The invention according to claim 1 wherein the damping means is an electrical network designed in accordance with prescribed transfer functions.

Claim 5

The invention according to claim 3 wherein the electrical network comprises: (a) a first means coupled to the first pickoff for multiplying the first pickoff signal by a factor p 1 ; (b) a second means coupled to the second pickoff for multiplying the second pickoff signal by a factor p 2 ; (c) a first integrator; (d) a third means coupled to the outputs of said first and second means, and to the output of a first integrator for summing said outputs; (e) a fourth means coupled to the output of said third means for multiplying said output by a factor a 1 ; (f) a fifth means coupled to the output of said third means for multiplying said output by a factor k z , the output of said fifth means providing the first torquer control signal; (g) a sixth means coupled to the first pickoff for multiplying the first pickoff signal by the factor p 1 ; (h) a seventh means coupled to the second pickoff for multiplying the second pickoff signal by the factor p 2 ; (i) a second integrator; (j) eighth means coupled to the outputs of said sixth and seventh means and to the output of said second integrator for summing the outputs of said sixth means, seventh means and second integrator; (k) ninth means coupled to the output of said eighth means for multiplying the output by the factor a 1 ; (l) tenth means coupled to the output of the said eighth means for multiplying the output by the factor k z , the output of said tenth means provided the second torquer control signal; (m) eleventh means coupled to the output of said eighth means for multiplying the output by a factor a 2 ; (n) twelfth means coupled to the output of said third means for multiplying said output by a factor a 2 ; (o) thirteenth means coupled to the input of said first integrator for summing the outputs of said fourth, fifth and eleventh means; and (p) fourteenth means coupled to the input of said second integrator for summing outputs of said ninth, tenth and twelfth means.

Claim 6

The circuit of claim 4 wherein each of said means for multiplying are implemented using scaled operational amplifiers.

Claim 7

In a two-axis gyroscope having mutually perpendicular first and second reference axes, a rotor with a spin axis, a first pickoff which produces a first pickoff signal whose magnitude is proportional to the angle the rotor spin axis makes with respect to the first reference axis, a second pickoff which produces a second pickoff signal whose magnitude is proportional to the angle the rotor spin axis makes with respect to the second reference axis, a first torquer which produces angular accelerations of the rotor about the first reference axis, a second torquer which produces angular accelerations of the rotor about the second reference axis, and control means for producing first and second torquer control signals from the first and second pickoff signals which control the amount of angular accelerations produced by the first and second torquers, respectively, the improvement comprising: the control means including damping means for stably damping variations in the magnitudes of the first and second pickoff signals occurring at the nutation frequency which damping means use the first and second pickoff signals to produce torquer control signals which cause substantial angular accelerations only when the first and second pickoff signal variations occur at the nutation frequency and which cause no angular accelerations when there are no variations in the magnitudes of the first and second pickoff signals at the nutation frequency, said damping means comprising an electric network including: (a) a first means coupled to the first pickoff for multiplying the first pickoff signal by a factor p 1 ; (b) a second means coupled to the second pickoff for multiplying the second pickoff signal by a factor p 2 ; (c) a first integrator; (d) a third means coupled to the outputs of said first and second means, and to the output of a first integrator for summing said outputs; (e) a fourth means coupled to the output of said third means for multiplying said output by a factor a 1 ; (f) a fifth means coupled to the output of said third means for multiplying said output by a factor k z , the output of said fifth means providing the first torquer control signal; (g) a sixth means coupled to the first pickoff for multiplying the first pickoff signal by the factor p 1 ; (h) a seventh means coupled to the second pickoff for multiplying the second pickoff signal by the factor p 2 ; (i) a second integrator; (j) eighth means coupled to the outputs of said sixth and seventh means and to the output of said second integrator for summing the outputs of said sixth means, seventh means and second integrator; (k) ninth means coupled to the output of said eighth means for multiplying the output by the factor a 1 ; (l) tenth means coupled to the output of the said eighth means for multiplying the output by the factor k z , the output of said tenth means providing the second torquer control signal; (m) eleventh means coupled to the output of said eighth means for multiplying the output by a factor a 2 ; (n) twelfth means coupled to the output of said third means for multiplying said output by a factor a 2 ; (o) thirteenth means coupled to the input of said first integrator for summing the outputs of said fourth, fifth and eleventh means; and (p) fourteenth means coupled to the input of said second integrator for summing outputs of said ninth, tenth and twelfth means.

Claim 8

In a two-axis gyroscope having mutually perpendicular first and second reference axes, a rotor with a spin axis, a first pickoff which produces a first pickoff signal whose magnitude is proportional to the angle the rotor spin axis makes with respect to the first reference axis, a second pickoff which produces a second pickoff signal whose magnitude is proportional to the angle the rotor spin axis makes with respect to the second reference axis, a first torquer which produces angular accelerations of the rotor about the first reference axis, a second torquer which produces angular accelerations of the rotor about the second reference axis, and control means for producing first and second torquer control signals from the first and second pickoff signals which control the amount of angular accelerations produced by the first and second torquers, respectively, the improvement comprising: the control means including damping means for stably damping variations in the magnitudes of the first and second pickoff signals occurring at the nutation frequency which damping means use the first and second pickoff signals to produce torquer control signals which cause substantial angular accelerations only when the first and second pickoff signal variations occur at the nutation frequency and which cause no angular accelerations when there are no variations in the magnitudes of the first and second pickoff signals at the nutation frequency, said damping means comprising an electric network including: (a) a first means coupled to the first pickoff for multiplying the first pickoff signal by a factor p 1 ; (b) a second means coupled to the second pickoff for multiplying the second pickoff signal by a factor p 2 ; (c) a first integrator; (d) a third means coupled to the outputs of said first and second means, and to the output of a first integrator for summing said outputs; (e) a fourth means coupled to the output of said third means for multiplying said output by a factor a 1 ; (f) a fifth means coupled to the output of said third means for multiplying said output by a factor k z , the output of said fifth means providing the first torquer control signal; (g) a sixth means coupled to the first pickoff for multiplying the first pickoff signal by the factor p 1 ; (h) a seventh means coupled to the second pickoff for multiplying the second pickoff signal by the factor p 2 ; (i) a second integrator; (j) eighth means coupled to the outputs of said sixth and seventh means and to the output of said second integrator for summing the outputs of said sixth means, seventh means and second integrator; (k) ninth means coupled to the output of said eighth means for multiplying the output by the factor a 1 ; (l) tenth means coupled to the output of the said eighth means for multiplying the output by the factor k z , the output of said tenth means providing the second torquer control signal; (m) eleventh means coupled to the output of said eighth means for multiplying the output by a factor a 2 ; (n) twelfth means coupled to the output of said third means for multiplying said output by a factor a 2 ; (o) thirteenth means coupled to the input of said first integrator for summing the outputs of said fourth, fifth and eleventh means; and (p) fourteenth means coupled to the input of said second integrator for summing outputs of said ninth, tenth and twelfth means.

Claim 9

The apparatus of claim 4 and further including capacitors coupling the outputs of said circuit to said torquers.

Claim 10

The circuit of claim 6 wherein each of said means for multiplying are implemented using scaled operational amplifiers.