Double rotation inertial measurement apparatus

• US 4,017,187 A
• Filed: 06/23/1975
• Issued: 04/12/1977
• Est. Priority Date: 06/23/1975
• Status: Expired due to Term

• Current Assignee: Sperry Rand Corporation (Unisys Corporation)
• Original Assignee: Sperry Rand Corporation (Unisys Corporation)
• Inventors: Schwartz, Bernard
• Primary Examiner(s): McGraw, Vincent P.
• Application Number:
  US05/589,319
• Time in Patent Office: 659 Days
• Field of Search: 356/106 LR
• US Class Current: 356/472
• CPC Class Codes: G01C 19/668 Assemblies for measuring along different axes, e.g. triads

Abstract

Apparatus for sensing movement with respect to mutually orthogonal axes includes a plurality of ring laser motion sensors, mounted so as to lie as if in planes which would define contiguous mutually perpendicular surfaces such as are found at a corner of a cube, wherein the cube is rotated constantly about a diagonal axis thereof. The rotation imparts equal components of rotation to each of the ring laser motion sensors, thereby eliminating the effects of mode locking and assuring that the beat frequencies obtained by heterodyning signals related to the contra-rotating light waves of each motion sensor are linearly related, over the operating range of the inertial device, to the components of rotational rate measured parallel to the input axes of the respective ring laser motion sensors. The rotating sensor system is supported along its spin axis in an inner gimbal member for rotation, in turn, about an outer or vertical axis perpendicular thereto. The effects of fixed or slowly changing bias errors are substantially cancelled in the system, any remaining drift about inertial or earth'"'"'s coordinate axes being substantially minimized by periodic reversal of the sense of rotation about the outer axis.

Claims

1. Inertial measurement apparatus comprising:

a plurality of equi-spaced ring laser means similarly disposed upon an inner spin member about a spin axis, thereof,

all of said ring laser means being disposed in individual planes at equal predetermined angles with respect to said spin axis,

spin motor means for rotating said inner spin member about said inner spin axis in a predetermined direction for eliminating mode-lock operation of each of said ring laser means within a predetermined operating range and whereby first components of bias and scale factor errors of the ring laser means outputs are cancelled,

drive frame means including first trunnion means for supporting said inner spin member therein,

reversible motor means for reversibly rotating said drive frame means about a second axis substantially perpendicular to said inner spin axis whereby second components of bias and scale factor errors of said ring laser means output are cancelled, and

fixed frame means including second trunnion means for supporting said drive frame means for reversible rotation about said second axis,

said reversible motor means serving to drive said drive frame means with respect to said fixed frame means through successive integral numbers of revolutions after respective successive reversals thereof.

2. Apparatus as described in claim 1 wherein said integral number is unity.

3. Apparatus as described in claim 1 additionally including acceleration sensor means mounted upon at least one of said inner spin member, said drive frame means, or said fixed frame means.

4. Apparatus as described in claim 1 wherein the respective sensitive axes of said ring laser means are substantially mutually orthogonal.

5. Apparatus as described in claim 3 wherein said acceleration sensor means includes first, second, and third accelerometer means having respective substantially mutually orthogonal sensitive first, second, and third axes and disposed upon said drive frame means for reversible rotation about said second axis.

6. Apparatus as described in claim 5 wherein said first accelerometer means sensitive axis is substantially parallel to said inner spin axis and said second accelerometer means sensitive axis is substantially parallel to said second axis whereby bias errors of said first and third accelerometer outputs are substantially cancelled.

7. Apparatus as described in claim 5 further including computer means responsive at least to first, second, and third of said plurality of ring laser means and to said first, second, and third accelerometer means.

8. Apparatus as described in claim 7 further including:

first pick-off means for providing a first measure of the instantaneous angular position of said inner spin member with respect to said drive frame means, and

second pick-off means for providing a second measure of the instantaneous angular position of said drive frame means with respect to said fixed frame means,

said computer means being additionally responsive to said first and second pick-off means.

9. Apparatus as described in claim 8 wherein said computer means comprises:

first coordinate rotator means responsive to said plurality of ring laser means for transforming the coordinates of the angular turn rate output signals thereof into coordinates associated with said inner spin axis,

rate corrector means responsive to said first coordinate rotator means for generating signals representative of angular rates of said inner spin member relative to earth'"'"'s coordinates, and

direction cosine integrator means responsive to said rate corrector means for generating signals representative of direction cosines of said inner spin member with respect to the said earth'"'"'s coordinates.

10. Apparatus as described in claim 9 wherein said computer means additionally includes:

second coordinate rotator means responsive to said direction cosine integrator means and to said first pick-off means, and

third coordinate rotator means responsive to said second coordinate rotator means and to said second pick-off means for generating signals representative of said direction cosine signals in craft coordinates.

11. Apparatus as described in claim 10 further comprising:

gimbal angle computer means responsive to said third coordinate rotator means for deriving signals representative craft azimuth, pitch, and roll angles, and

craft navigation display means responsive to said gimbal angle computer means.

12. Apparatus as described in claim 10 further comprising:

acceleration transformer means responsive to said first, second, and third accelerometer means and selectively to said second coordinate rotator means, said third coordinate rotator means, or to said direction cosine integrator means for generating signals representative of craft acceleration in earth'"'"'s coordinates,

said first coordinate rotator means being further responsive to said acceleration transformer means.