Control system for angular displacement sensor

• US 3,992,952 A
• Filed: 12/20/1974
• Issued: 11/23/1976
• Est. Priority Date: 12/20/1974
• Status: Expired due to Term

• Current Assignee: Kearfott Guidance and Navigation Corporation
• Original Assignee: Singer Company (SVP Holdings Ltd.)
• Inventors: Friedland, Bernard, Hutton, Maurice F.
• Primary Examiner(s): Goldstein, Herbert
• Application Number:
  US05/534,615
• Time in Patent Office: 704 Days
• Field of Search: 73/505, 73/517 AV, 73/DIG. 1
• US Class Current: 73/504.14
• CPC Class Codes: G01C 19/5691 of essentially three-dimensional vibrators, e.g. wine glass-type vibrators

Abstract

Stable reference gyroscopic apparatus is provided in the form of an angular displacement sensor which employs an end-supported vibratory rod or wire, instead of the commonly used rotatable element. The apparatus of the invention incorporates an improved means for maintaining the vibrational amplitude of the center of the vibratory element constant, and electronic circuit means for causing the orbit of center of the vibratory element to remain in a straight line, both means being effective to eliminate the major sources of potential drift in the sensor.

Claims

1. Gyroscopic apparatus including:

a casing;

first and second support means mounted in said casing;

an elongated vibratory element having its ends supported in said first and second support means and extending between said support means in said casing;

first drive means mounted adjacent said vibratory element at a point intermediate the ends thereof and responsive to electric drive signals for creating drive forces for the center of said vibratory element along a first axis traversing the longitudinal axis of the vibratory element;

second drive means mounted adjacent said vibratory element at the intermediate point thereon and responsive to electric drive signals for producing drive forces for the center of said vibratory element along a second axis traversing the longitudinal axis of the vibratory element;

first pickoff means mounted adjacent said vibratory element for sensing linear motion of the center of said vibratory element along said first axis and for producing pickoff signals corresponding thereto;

second pickoff means mounted adjacent said vibratory element for sensing linear motion of the center thereof along said second axis and for producing pickoff signals corresponding thereto; and

electronic control circuitry connected to said pickoff means and responsive to the pickoff signals produced thereby to develop signals representative of the position and velocity of the center of the vibratory element along the first and second axis at any instant said control circuitry responding to said position and velocity signals to produce drive signals for said drive means so as to permit maintaining an amplitude of vibration of the center of said element essentially constant in any given direction and to force the ellipticity of the vibrational path of the center of said element essentially to zero, said electronic control circuitry comprising;

a. first means to develop a first signal which is the square of the velocity along said first axis;

b. second means to develop a second signal which is the square of the velocity along said second axis;

c. third means for developing a third signal which is the square of the position along said first axis;

d. fourth means for developing a signal which is the square of the position along said second axis;

e. fifth means for multiplying the signal representing the velocity along said first axis by the signal representing the position along said second axis to develop a fifth signal;

f. sixth means for multiplying the signal representing velocity along said second axis by the signal representing position along said first axis to develop a sixth signal;

g. seventh means for subtracting said fifth signal from said sixth signal to develop a seventh signal;

h. eighth means for adding said first and second signals to develop an eighth signal;

i. ninth means for adding said third and fourth signals to develop a ninth signal;

j. tenth means for multiplying said eighth signal by a constant gain to develop a tenth signal;

k. eleventh means for adding said tenth and ninth signals to develop an eleventh signal;

l. means for providing a reference signal;

m. twelfth means for subtracting said reference signal from said eleventh signal to develop a twelfth signal;

n. thirteenth means for filtering said twelfth signal to develop a thirteenth signal;

o. fourteenth means having said thirteenth signal as an input for developing a fourteenth signal which is the negative sum of said thirteenth signal times a first constant and the integral of said thirteenth signal times a second constant;

p. fifteenth means for multiplying said fourteenth signal by said signal representing velocity along said first axis to develop a fifteenth signal;

q. sixteenth means for multiplying said fourteenth signal by said signal representing velocity along said second axis to develop a sixteenth signal;

r. seventeenth means for filtering said seventh signal to develop a seventeenth signal;

s. eighteenth means having said seventeenth signal as an input for developing an eighteenth signal which is the sum of said seventeenth signal times a constant and the integral of said seventeenth signal times a constant;

t. Nineteenth means for multiplying said eighteenth signal by said signal representing position along said second axis to develop a nineteenth signal;

u. twentieth means for multiplying said eighteenth signal by the signal representing position along said first axis;

v. twenty-first means for adding said fifteenth and nineteenth signals to produce a drive signal for said first axis; and

w. twenty-second means for subtracting said twentieth signal from said sixteenth signal to produce a drive signal for said second axis.

2. The gyroscopic apparatus defined in claim 1, in which said first and second drive means respectively comprise first and second pairs of capacitor drive electrodes diametrically mounted in said casing on opposite sides of said vibratory element.

3. The gyroscopic apparatus defined in claim 2, in which said pickoff means respectively comprise first and second pairs of capacitor pickoff electrodes diametrically mounted in said casing on opposite sides of said vibratory element.

4. The gyroscopic apparatus defined in claim 3, in which the first and second axes are disposed perpendicular to one another so that said drive electrodes create electrostatic forces for the center of the vibratory element in two orthogonal directions, and so that said pickoff electrodes sense linear motions of the center of the vibratory element in said two orthogonal directions.

5. The gyroscopic apparatus defined in claim 1, in which the pickoff means are displaced from the drive means along the longitudinal axis of said vibratory element, and in which said first and second axes are disposed perpendicular to the longitudinal axis and to one another.

6. Apparatus according to claim 1 wherein each of said fourteenth and eighteenth means comprise:

a. a first constant gain circuit;

b. a second constant gain circuit having its input tied to that of the first circuit;

c. an integrator having as its input the output of said first constant gain circuit; and

d. summing means having as inputs the outputs of said integrator and said second constant gain circuit.