SYSTEM AND METHOD FOR ROLL ANGLE INDICATION AND MEASUREMENT IN FLYING OBJECTS

• US 20120199690A1
• Filed: 11/22/2009
• Published: 08/09/2012
• Est. Priority Date: 03/02/2009
• Status: Active Grant

• Current Assignee: Omnitek Partners LLC
• Original Assignee: Omnitek Partners LLC
• Inventors: Rastegar, Jahangir S., Pereira, Carlos M.
• Granted Patent: US 8,258,999 B2
• Time in Patent Office: Days
• US Class Current: 244/3.19
• CPC Class Codes: F41G 7/305 for spin-stabilized missiles
• CPC Class Codes: F42B 15/01 Arrangements thereon for guidance or control steering arrangements F42B10/60; aircraft flight control B64C; guidance systems other than those installed aboard F41G7/00, F41G9/00; locating by use of radio or other waves G01S; flight control in general G05D1/00; computer aspects G06]
• CPC Class Codes: G01B 21/22 for measuring angles or tapers; for testing the alignment of axes

Abstract

A method for onboard determination of a roll angle of a projectile. The method including: transmitting a polarized RF signal from a reference source, with a predetermined polarization plane; receiving the signal at a pair of polarized RF sensor cavities positioned symmetrical on the projectile with respect to the predetermined polarization plane; receiving the signal at a third polarized RF sensor cavity positioned such that it receives a maximum signal at zero roll angle positioning; differentiating between up or down positioning of the desired roll angle position based on an output from a fourth sensor on the projectile; analyzing an output of the pair of polarized RF sensor cavities and the third RF sensor cavity resulting from the received signal and an output of the fourth sensor; generating a curve based on the output of the pair of polarized RF sensor cavities and the third RF sensor cavity indicating a relationship between roll angle and the third sensor output; and determining a roll angle positioning of the projectile based on the curve.

Claims

1. A method for onboard determination of a roll angle of a projectile, the method comprising:

transmitting a polarized RF signal from a reference source, with a predetermined polarization plane;

receiving the signal at a pair of polarized RF sensor cavities positioned symmetrical on the projectile with respect to the predetermined polarization plane;

receiving the signal at a third polarized RF sensor cavity positioned such that it receives a maximum signal at zero roll angle positioning;

differentiating between up or down positioning of the desired roll angle position based on an output from a fourth sensor on the projectile;

analyzing an output of the pair of polarized RF sensor cavities and the third RF sensor cavity resulting from the received signal and an output of the fourth sensor;

generating a curve based on the output of the pair of polarized RF sensor cavities and the third RF sensor cavity indicating a relationship between roll angle and the third sensor output; and

determining a roll angle positioning of the projectile based on the curve.

2. The method of claim 1, further comprising controlling the projectile based on the determined roll angle positioning.

3. The method of claim 1, wherein the predetermined polarization plane is vertical.

4. The method of claim 1, wherein the fourth sensor is selected from a group consisting of a gravity switch, inclinometer, GPS receiver, and another polarized RF reference source.

5. The method of claim 1, wherein the generating step comprises using the output of the pair of polarized RF sensor cavities and the third RF sensor cavity to make the curve fitting more accurate and reduce the effects of noise and measurement error.

6. The method of claim 1, further comprising:

receiving the signal at one or more additional polarized RF sensor cavities positioned at different roll angle locations on the projectile;

analyzing an output of the additional polarized RF sensor cavities resulting from the received signal; and

the generating step includes generating the curve based on the output of the additional polarized RF sensor cavities to make the curve more accurate and reduce the effect of noise and measurement errors.

7. The method of claim 1, wherein where the projectile spins with constant or slow varying speed and spin rates, the method further comprises scaling of the roll angle curve to interpolate the role angle scaling between scaling events.

8. The method of claim 1, wherein a speed or position of the projectile is known, the method further comprises scaling of the roll angle curve and using the curve to interpolate the scaling of the profile between zero roll angle scaling events.

9. The method of claim 1, wherein where the projectile is not spinning or has highly variable spinning, the method further comprises scaling of the roll angle curve and maneuvering the projectile at certain time intervals to zero roll angle positioning for scaling and updating the generated curve.

10. A projectile comprising:

a casing;

a pair of polarized RF sensor cavities positioned symmetrically on the casing with respect to a predetermined polarization plane;

a third polarized RF sensor cavity positioned on the casing such that it receives a maximum signal at zero roll angle positioning;

a fourth sensor positioned on the casing; and

a processor configured to;

analyze an output of the pair of polarized RF sensor cavities and the third RF sensor cavity resulting from the received signal and the fourth sensor;

generate a curve based on the output of the pair of polarized RF sensor cavities and the third RF sensor cavity indicating a relationship between roll angle and the third sensor output; and

determine a roll angle positioning of the projectile based on the curve.