Adaptive bias for electrically suspended gyroscope
AssigneeHoneywell Inc.
InventorRobert C. Staats
Life of this patent
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Abstract
Means for varying the preload bias forces in the suspension system of an electrostatic gyroscope as a function of acceleration forces to which the gyroscope is subjected. Under zero acceleration environment, the preload bias forces are maintained at a low level to keep at a minimum the errors due to gyro drift introduced by bias forces. With an increase in acceleration, bias forces are automatically increased, thereby providing the gyroscope with high "g" capability without sacrificing low "g" performance.
Claims6
Apparatus for supplying electric charge to a pair of electrodes supporting the inertial member of an inertial instrument along an axis, said apparatus comprising:
- position sensing means for detecting displacement of said inertial member along said axis and for generating an error signal as a function of said displacement;
- means for generating a bias charge signal and supplying said bias charge signal to each of said electrodes;
- means for generating a control charge signal function of said error signal and adding said control charge signal to the bias charge signal at one of said electrodes while subtracting said charge signal from the bias charge signal at the other of said electrodes;
- and
- means for varying the bias charge as a function of said control charge such that the resulting charge on one of the electrodes is substantially equal to twice the bias charge, while the resulting charge on the other of said electrodes is substantially equal to zero.
In an inertial instrument wherein an inertial member is maintained in suspension along an axis, between first and second electrodes positioned at substantially opposite sides of said member, and wherein means are provided for generating electric charge at said electrodes to produce said electric forces, said means for generating electric charges comprising:
- first and second charge amplifiers connected to supply electric charge to said first and second electrodes, respectively, said first and second amplifiers having a common mode input and a differential mode input;
- means for sensing the displacement of the inertial member from a preferred position along said axis and for generating a position error signal;
- a bias signal generating means for supplying a bias signal to the common mode input of said first and second amplifiers;
- control signal generating means for providing a control signal as a function of said position error signal and to supply said control signal to the differential mode input of said first and second amplifiers;
- and
- means for varying the amplitude of said bias signal as a function of the position error signal such that upon displacement of said inertial member from the preferred position, the charge supplied by one of said charge amplifiers is substantially zero and the charge supplied by the other of said charge amplifiers is in the amount required to generate a force necessary to return the inertial member to its preferred position.
In an inertial instrument wherein a substantially spherical inertial member is maintained in suspension between a plurality of pairs of electrodes by means of electric forces, each said pair consisting of first and second electrodes positioned along an axis at diametrically opposite sides of said member and wherein means are provided for generating electric charges to produce said electric forces, said means for generating electric charges for each pair of electrodes comprising:
- first and second charge amplifiers connected to supply electric charge to said first and second electrodes, respectively, said first and second amplifiers having a common mode input and a differential mode input;
- means for sensing the displacement of the inertial member from a preferred position along the axis of said pair and for generating a position error signal;
- a bias signal generating means for supplying a bias signal to the common mode input of said first and second amplifiers;
- control signal generating means for providing a control signal as a function of said position error signal and to supply said control signal to the differential mode input of said first and second amplifiers;
- and
- means for varying the amplitude of said bias signal as a function of the position error signal such that upon displacement of said inertial member from the preferred position, the charge supplied by one of said charge amplifiers is substantially zero and the charge supplied by the other of said charge amplifiers is in the amount required to generate a force necessary to return the inertial member to its preferred position.
Dependencies are inferred from the claim text.