Linear and rotational accelerometer

• US 5,831,164 A
• Filed: 01/21/1997
• Issued: 11/03/1998
• Est. Priority Date: 01/21/1997
• Status: Expired due to Fees

• Current Assignee: Conrad Technologies Incorporated
• Original Assignee: Conrad Technologies Incorporated
• Inventors: DeCleene, Donald F., Reddi, M. Mahadeva
• Primary Examiner(s): Williams, Hezron E.
• Assistant Examiner(s): MOLLER, RICHARD ALAN
• Application Number:
  US08/786,774
• Time in Patent Office: 651 Days
• Field of Search: 73/514.01, 73/514.02, 73/510, 73/514.16, 73/514.17, 73/514.18, 73/514.21, 73/514.22, 73/514.23, 73/514.24, 73/514.32 , 73/514.35, 73/514.36, 73/514.37, 73/514.38, 73/1.38, 340/669
• US Class Current: 73/514.01
• CPC Class Codes: G01P 15/0888 for indicating angular acceleration
• CPC Class Codes: G01P 15/125 by capacitive pick-up
• CPC Class Codes: G01P 15/131 with electrostatic counterbalancing means
• CPC Class Codes: G01P 15/18 in two or more dimensions
• CPC Class Codes: G01P 2015/0831 the mass being of the paddle type having the pivot axis between the longitudinal ends of the mass, e.g. see-saw configuration

Abstract

A two degree of freedom (2 DOF) accelerometer comprising two imbalanced sensing modules (i.e., bar modules having an unbalance) is provided such that two sensing modules are located in the plane to be measured. The two imbalanced sensing modules have force balance and are used to measure linear and angular accelerations in two degrees of freedom. A single modular design is used for both of the axes. Each of the two individual sensing modules has a housing containing a proof mass for each measured output and a support of the proof mass with the support optimized for the sensitive axis selected for sensor output and having high rigidity in all other axes of the support. Also provided is electrostatic servo force balance technology. A proportional-integral-derivative (PID) controller is used to obtain a closed loop bandwidth of 1 kHz and a steady state error of zero for full scale accelerations up to 75 g'"'"'s and 1000 rad/sec².

Claims

1. An accelerometer comprising:

a plurality of sensing modules for determining linear and angular accelerations in a plurality of degrees of freedom, each sensing module comprising;

a housing;

a proof mass having a dimension, a shape, a mass, and a center of gravity, said proof mass mounted displaced from said center of gravity by an amount which produces a displacement response to both linear and angular acceleration;

a support for connecting said proof mass to said housing; and

detection means for detecting said displacement response of said proof mass.

2. An accelerometer according to claim 1, wherein said proof mass is a substantially rectangular bar.

3. An accelerometer according to claim 1, wherein said dimension is a length and said amount which produces said mass imbalance is small relative to said length of said proof mass.

4. An accelerometer according to claim 1, further comprising processing circuitry including electrostatic force balancing means for balancing inertial forces and measuring means for measuring a force required to balance said proof mass.

5. An accelerometer according to claim 4, wherein the electrostatic force balancing is pulse width modulated.

6. An accelerometer according to claim 1, wherein the dimension, the shape and the mass of said proof mass in each sensing module are substantially the same.

7. An accelerometer according to claim 1, wherein said detection means includes a plurality of capacitors, each capacitor having substantially the same construction and comprising a fixed electrode located opposite to a surface of said proof mass.

8. An accelerometer according to claim 1, wherein said support comprises two in line hinges on opposite sides of said proof mass.

9. An accelerometer according to claim 1, wherein said support comprises a torsional bar.

10. An accelerometer according to claim 1, wherein said support comprises bearing supports.

11. An accelerometer according to claim 1, wherein said plurality of sensing modules are coupled into pairs, each pair of sensing modules detecting movement in two degrees of freedom in a plane.

12. An accelerometer according to claim 11, wherein said plurality of sensing modules consists of two sensing modules for detecting movement in two degrees of freedom in a plane.

13. An accelerometer according to claim 11, wherein said plurality of sensing modules consists of four sensing modules for detecting movement in four degrees of freedom.

14. An accelerometer according to claim 11, wherein said plurality of sensing modules consists of six sensing modules for detecting movement in six degrees of freedom.

15. An accelerometer comprising:

a pair of sensing modules for determining linear and angular accelerations in two degrees of freedom, each sensing module comprising;

a housing;

a proof mass having a dimension, a shape, a mass, and a center of gravity, said proof mass mounted displaced from said center of gravity by an amount which produces a displacement response to both linear and angular acceleration;

a support for connecting said proof mass to said housing;

detection means for detecting said displacement response of said proof mass; and

processing circuitry for receiving a first signal indicative of angular and linear acceleration imposed on said proof mass and responsive to a second signal generated by a second sensing module which is substantially the same as the first sensing module to generate a measure of linear acceleration and a measure of angular acceleration;

wherein the pair of sensing modules is located in a plane for measuring motion in the two degrees of freedom.

16. An accelerometer according to claim 15, wherein said sensing modules are substantially the same.

17. An accelerometer comprising:

three pairs of sensing modules for determining linear and angular accelerations in six degrees of freedom, each sensing module comprising;

a housing;

a proof mass having a dimension, a shape, a mass, and a center of gravity, said proof mass mounted displaced from said center of gravity by an amount which produces a displacement response to both linear and angular acceleration;

a support for connecting said proof mass to said housing;

detection means for detecting said displacement response of said proof mass; and

processing circuitry for receiving a first signal indicative of angular and linear acceleration imposed on said proof mass and responsive to a second signal generated by a second sensing module which is substantially the same as the first sensing module to generate a measure of linear acceleration and a measure of angular acceleration;

wherein each of the three pairs of sensing modules is located in a different mutually intersecting plane for measuring the six degrees of freedom.

18. An accelerometer comprising a plurality of substantially similar sensing modules for determining linear and angular accelerations in a plurality of degrees of freedom, each sensing module comprising:

a housing;

a proof mass having a dimension, a shape, a mass, and a center of gravity, said proof mass mounted displaced from said center of gravity by an amount which produces a displacement response to both linear and angular acceleration;

a support having two opposed hinges on opposite sides of said proof mass for connecting said proof mass to said housing;

detection means having a plurality of substantially similar capacitors comprising a fixed electrode located opposite to a surface of said proof mass for detecting said displacement response of said proof mass; and

processing circuitry for receiving a first signal indicative of angular and linear acceleration imposed on said proof mass and responsive to a second signal generated by a second sensing module which is substantially the same as the first sensing module to generate a measure of linear acceleration and a measure of angular acceleration.

19. An accelerometer comprising:

three pairs of substantially similar sensing modules in three different planes for determining linear and angular accelerations in six degrees of freedom, each sensing module comprising;

a housing;

a proof mass having a dimension, a shape, a mass, and a center of gravity, said proof mass mounted displaced from said center of gravity by an amount which produces a displacement response to both linear and angular acceleration;

a support having two opposed hinges on opposite sides of said proof mass for connecting said proof mass to said housing;

detection means having a plurality of substantially similar capacitors comprising a fixed electrode located opposite to a surface of said proof mass for detecting said displacement response of said proof mass; and

processing circuitry for receiving a first signal indicative of angular and linear acceleration imposed on said proof mass and responsive to a second signal generated by a second sensing module which is substantially the same as the first sensing module to generate a measure of linear acceleration and a measure of angular acceleration.