Real time boresight error slope sensor

• US 6,079,666 A
• Filed: 04/25/1986
• Issued: 06/27/2000
• Est. Priority Date: 04/25/1986
• Status: Expired due to Fees

• Current Assignee: Alton B Hornback
• Original Assignee: Alton B Hornback
• Inventors: Hornback, Alton B.
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): Wesson, Theresa M.
• Application Number:
  US06/859,033
• Time in Patent Office: 5,177 Days
• Field of Search: 244/3.19, 244/3.15, 244/3.16
• US Class Current: 244/3.19
• CPC Class Codes: F41G 7/2213 maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
• CPC Class Codes: F41G 7/2246 Active homing systems, i.e. comprising both a transmitter and a receiver
• CPC Class Codes: F41G 7/2253 Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
• CPC Class Codes: F41G 7/2286 using radio waves

Abstract

In a missile which employs a terminal homing seeker and a proportional navigation guidance law the space rate of change of boresight error, i.e., the boresight error slope, is one of the predominant error sources.

It has been found that the boresight error slope is proportional to the curvature of the seeker open loop transfer characteristic. Accordingly, the boresight error slope sensor senses the curvature of the seeker open loop transfer characteristic. This is accomplished by intermittently dithering the seeker instantaneous field-of-view about the line of sight at a rate too great for the normal tracking loop to respond. Thus the open loop transfer characteristic is obtained while leaving the normal tracking loop unperturbed. The curvature of the open loop transfer characteristic is then obtained in real time by computing the "second differences" from the measured open loop transfer characteristic.

Claims

1. A boresight error slope reduction system for sensing, in real time, a boresight error slope in a homing seeker, said system comprising:

(a) a seeker having a steerable field-of-view, said field-of-view having an electrical boresight axis, and

(b) a receiver wherein a wide bandwidth video signal voltage is obtained when an object is within said field-of-view, said object being on a line-of-sight from said seeker causing an included angle between said line-of-sight and said boresight axis, said video signal voltage being a function of said included angle, and

(c) a tracking loop having a means for using said signal voltage to steer said field-of-view so that said object remains within said field-of-view and a means for generating a low-pass filtered dynamic lag voltage from said video signal voltage, and

(d) a dither waveform generator wherein a dither voltage is generated and

(e) a means for using said dither voltage to cause a dither of said boresight axis and

(f) a means for causing said tracking loop to be open during said dither of said boresight axis and

(g) a boresight error slope computer circuit for generating a transfer characteristic having a measurable curvature, said transfer characteristic being a voltage functionally related to said included angle, said angle resulting from said dither, and

(h) a boresight error slope computer circuit for generating a correction voltage, said correction voltage being a function of said curvature of said transfer characteristic in a neighborhood of said line of sight, and

(i) an additive means for using said correction voltage to reduce said boresight error slope.

2. The boresight error slope reduction system of claim 1 wherein said tracking loop includes an automatic gain control amplifier and an automatic gain control computer, said automatic gain control computer comprising:

(a) a transfer characteristic sample-and-hold circuit for obtaining two samples of said transfer characteristic, a first sample being obtained at a first instant, said first instant being the instant of coincidence between said wide bandwidth video signal voltage and said low-pass filtered dynamic lag voltage, and a second sample being obtained at a second instant, said second instant being at a different time from said first instant, and

(b) a signal subtracter circuit for generating a direct current signal voltage by subtracting said first sample of said transfer characteristic from said second sample of said transfer characteristic and

(c) a dither sample-and-hold circuit for obtaining two samples of said dither voltage, a first sample of said dither voltage being obtained at said first instant and a second sample of said dither voltage being obtained at said second instant, and

(d) a dither subtracter circuit for generating a direct current reference voltage by subtracting said first sample of said dither voltage from said second sample of said dither voltage and

(e) an automatic gain control subtracter circuit for generating an automatic gain control voltage by subtracting said direct current reference voltage from said direct current signal voltage and

(f) a means for applying said automatic gain control voltage to said automatic gain control amplifier.

3. The boresight error slope reduction system of claim 1 wherein said seeker is a radio frequency seeker having a phase sensing monopulse antenna and said additive means is a phase shifter.

4. The boresight error slope reduction system of claim 1 wherein said seeker is an infra-red seeker and said additive means is an adder circuit for adding said correction voltage to said dynamic lag voltage.