Millimeter wave length guidance system

• US 4,665,401 A
• Filed: 10/10/1980
• Issued: 05/12/1987
• Est. Priority Date: 10/10/1980
• Status: Expired due to Term

• Current Assignee: Alliant Techsystems Incorporated (Northrop Grumman Corporation)
• Original Assignee: Sperry Corporation (Unisys Corporation)
• Inventors: Gregg, Jack E., Garrard, John T., Roeder, Robert S.
• Primary Examiner(s): Tubbesing, T. H.
• Application Number:
  US06/195,809
• Time in Patent Office: 2,405 Days
• Field of Search: 343/5 VQ, 343/7.4, 343/7.3, 343/7.5, 343/14, 342/75, 342/85, 342/87, 342/128
• US Class Current: 342/75
• CPC Class Codes: F41G 7/2246 Active homing systems, i.e. comprising both a transmitter and a receiver
• CPC Class Codes: F41G 7/2286 using radio waves
• CPC Class Codes: G01S 13/68 for angle tracking only
• CPC Class Codes: G01S 13/72 for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar

Abstract

A high frequency target seeking device, using a stabilized reflector antenna, performs range search and tracking functions and target angle search and tracking functions. A technique is provided for target range discrimination using several narrow band i.f. filters, also thereby improving signal-to-clutter ratio and signal-to-receiver noise ratio. Target search is accomplished with simultaneous range and antenna azimuth scanning, with the range bins and the antenna beam swept across the target. A multiplexer selects the range bin having signals indicative of the target. Target range tracking is accomplished by the multiplexer additionally automatically selecting range bins adjacent to the target'"'"'s range bin and comparing their output signals. Antenna stabilization is accomplished utilizing signals from vehicle pitch, roll, and yaw rate sensors, and antenna elevation and azimuth rate and angle sensors. These signals are processed in the antenna control circuit according to predetermined relationships to provide the desired antenna stabilization.

Claims

1. High frequency, vehicle coupled, target detecting seeker system having search and track modes and having twist reflector antenna means coupled to receiver means comprising:

a high frequency target sensor system having search and track modes coupled to said receiver means for detecting the position and range of said target and for providing target range signals, and signals Kε

_e representative of the difference between said antenna'"'"'s actual and desired line of sight rates of angular change with respect to a first predetermined reference in a first direction, and signals Kε

_a representative of the difference of said antenna'"'"'s actual and desired line of sight rate of angular change with respect to said first predetermined direction in a second direction orthogonal to said first direction, and for further providing signals λ

_del representative of said antenna'"'"'s desired line of sight angle with respect to said first predetermined reference in said first direction and signals λ

_daz representative of said antenna'"'"'s desired line of sight angle with respect to said first predetermined reference in said second direction;

antenna drive means coupled to said twist reflector antenna means and coupled to said target sensor system means for positioning said antenna in said first and second directions according to said target sensor system signals;

first angle sensor means coupled to said antenna drive means for providing signals β

representative of said antenna drive means angle in said first direction with respect to said first predetermined reference;

second angle sensor means coupled to said antenna drive means for providing signals ψ

representative of said antenna drive means angle in said second direction with respect to said first predetermined reference;

first vehicle rate sensor means coupled to said vehicle for providing signals θ

_p representative of the angular rate of change of said vehicle in a third direction with respect to a second predetermined reference;

second vehicle rate sensor means coupled to said vehicle for providing signals φ

HD R representative of the angular rate of change of said vehicle in a fourth direction orthogonal to said third direction, with respect to said predetermined reference;

third vehicle rate sensor means coupled to said vehicle for providing signals φ

_y representative of the angular rate of change of said vehicle in a fifth direction orthogonal to said third and fourth directions, with respect to said second predetermined reference; and

antenna control means coupled to said antenna drive means and adapted to receive said signals Kγ

_e, Kε

_a, θ

_p, φ

_R, θ

_y, β

, ω

, λ

_daz and λ

_del for providing signals in said track mode for controlling said antenna drive means rate of angular change β

in said first direction substantially according to the formula;

space="preserve" listing-type="equation">β

=1/2(Kε

.sub.e -θ

.sub.p +2ψ

φ

.sub.R)

and for further providing signals in said track mode for controlling said antenna drive means angular rate of change ψ

in said second direction substantially according to the formula;

space="preserve" listing-type="equation">ψ

=1/2(Kε

.sub.a -θ

.sub.y -2β

φ

.sub.R)

and for providing signals in said search mode for controlling said antenna drive means angular rate of change β

in said first direction substantially according to the formula;

space="preserve" listing-type="equation">β

=1/2[K(-∫

(θ

.sub.p. -2φ

.sub.R ψ

)dt+λ

.sub.del -2β

)-(θ

.sub.p -2φ

.sub.R ψ

)]

and for further providing signals in said search mode for controlling said antenna drive means angular rate of change ψ

in said second direction substantially according to the formula;

space="preserve" listing-type="equation">3/8=1/2[K(-∫

(φ

.sub.y +2β

φ

.sub.R)dt+λ

.sub.daz -2ψ

)-(φ

.sub.y+ 2β

φ

.sub.R)].

4. The invention according to claims 1 or 3 wherein said first direction is the antenna elevation direction and said second direction is the antenna azimuth direction;

and

said antenna drive means comprises;

an elevation servomotor coupled to said twist reflector antenna for positioning said antenna in said elevation direction; and

azimuth servomotor coupled to said twist reflector antenna means for positioning said antenna in said azimuth direction;

first rate sensor means coupled to said antenna drive means for providing signals β

representative of said antenna drive means angular rate of change in said elevation direction;

second rate sensor means coupled to said antenna drive means for providing signals ψ

representative of said antenna drive means angular rate of change in said azimuth direction;

first tachometer summing amplifier means having input means responsive to said antenna control means signals and said first rate sensor means signals, and coupled to said elevation servomotor means, for comparing said antenna control means signals and first rate sensor means signals, to derive an error signal equal to the difference between said input signals for controlling said elevation servomotor; and

second tachometer summing amplifier means having input means responsive to said antenna control means signals and said first rate sensor means signals, and coupled to said azimuth servomotor means, for comparing said antenna control means signals and second rate sensor means signals to derive an error signal equal to the difference between said input signals for controlling said azimuth servomotor means.

5. The invention according to claim 4 wherein:

said first rate sensor means comprises a tachometer;

said second rate sensor means comprises a tachometer;

said first angle sensor means comprises a variable resistance coupled to said elevation servomotor having an output signal proportional to the angle of said elevation servomotor; and

said second angle sensor comprises a variable resistance coupled to said azimuth servomotor and having an output representative of the angle of said azimuth servomotor.

6. The invention according to claims 1 or 3 wherein said third, fourth, and fifth directions correspond to said vehicle'"'"'s pitch, roll, and yaw directions, respectively, and

said first vehicle rate sensor means comprises a pitch rate gyroscope;

said second vehicle rate sensor means comprises a roll rate gyroscope; and

said third vehicle rate sensor means comprises a yaw rate gyroscope.

7. The invention according to claims 1 or 3 wherein said antenna control means comprises:

first multiplier means coupled to said second vehicle rate sensor means and to said second angle sensor means for multiplying said second rate signal by said second angle signal and for providing an output signal representative thereof;

first vehicle rate amplifier coupled to said first vehicle rate sensor and to said first multiplier for subtracting said first multiplier output signal from said first rate signal and for providing an output signal representative thereof;

first rate summing amplifier switchably responsive to said signal Kε

_e and coupled to said first vehicle rate amplifier for subtracting therefrom said output signal of said first vehicle rate amplifier, and multiplying said difference by 0.5, and for providing an output signal representative thereof;

first integrator means coupled to said first vehicle rate amplifier for integrating the output signal of said first vehicle rate amplifier, and for providing an output signal representative thereof;

first angle amplifier adapted to receive said signal λ

_del, coupled to said first integrator and to said first angle sensor means, for multiplying said first angle sensor means output signal by two and subtracting the multiplication result from the difference of said signal λ

_del and said first integrator output signal, for further multiplying the subtraction result by a constant K, and for further providing an output signal therefrom switchably coupled to said first rate summing amplifier;

second multiplier means coupled to said second vehicle rate sensor means and to said first angle sensor means for multiplying said second rate signal by said first angle signal and for providing an output signal representative thereof;

second vehicle rate amplifier coupled to said third vehicle rate sensor and to said second multiplier for adding said second multiplier output signal from said third rate signal and for providing an output signal representative thereof;

second rate summing amplifier switchably responsive to said Kε

_a and coupled to said second vehicle rate amplifier for subtracting therefrom said output signal of said second vehicle rate amplifier, and multiplying said difference by 0.5, and for providing an output signal representative thereof;

second integrator means coupled to said second vehicle rate amplifier for integrating the output signal of said second vehicle rate amplifier, and for providing an output signal representative thereof; and

second angle amplifier adapted to receive said search command signal λ

_del, coupled to said second integrator and to said second angle sensor means, for multiplying said second angle sensor means output signal by two and subtracting the multiplication result from the difference of said signal λ

_daz and said first integrator output signal, for further multiplying the subtraction result by said constant K, and for further providing, an output signal therefrom switchably coupled to said second rate summing amplifier.

8. The invention according to claim 7 further comprising:

first switch means having a first input means coupled to said first angle amplifier, second input means adapted to receive said signal Kε

_e and output means coupled to said first rate amplifier for switchably coupling said output means of said switch means to said input means of said first switch means;

16. The apparatus of claims 1, 2 or 3 including means for providing said target range signals as an automatic gain control signal to said receiver means.

2. A high frequency target sensor system having search and track modes and having directive antenna means coupled to receiver means comprising:

transmitter oscillator means coupled to said directive antenna means for illumination of targets and background by said directive antenna means, and further coupled to said receiver means for generating therein a beat frequency signal in the presence of said illuminated target or background;

transmitter oscillator drive means having input terminals and output terminals, said output terminals being coupled to said transmitter oscillator for providing transmitter oscillator drive signals at said output terminals responsive to the amplitude of signals applied to said input terminals, the frequency of said transmitter oscillator signals being responsive to said transmitter oscillator drive signals;

a plurality of range bin means coupled to receive said beat frequency signal, each of said range bins being responsive to illuminated objects in substantially contiguous predetermined ranges and for providing output signals from a bin corresponding to the range of said illuminated target, and for further providing signals from bins corresponding to ranges adjacent to said target range;

difference means having input terminals coupled to receive said signals corresponding to ranges adjacent to said target, for providing in said tracking mode signals representative of the difference in amplitude of said adjacent range bin signals to said oscillator drive means;

frequency discrimination means having input means coupled to receive said beat frequency signal and having an output means coupled to said transmitter oscillator drive means for providing in said tracking mode, background range tracking signals to said transmitter drive means upon departure of said beat frequency from a predetermined frequency value;

range search generator means switchably coupled to said transmitter oscillator drive means for providing in said search mode range search signals;

antenna drive means having input terminals and being coupled to said directive antenna means, for varying the position of said directive antenna means in space in response to signals applied to said antenna drive means input terminals;

angle track demodulator means having input terminals coupled to receive said target range bin signal and output terminals, for providing signals Kε

_e representative of the difference between said antenna'"'"'s actual and desired line of sight rate of angular change with respect to a first predetermined reference in a first direction, and signals Kε

_a representative of the difference between said antenna'"'"'s actual and desired line of sight rate of angular change with respect to said first predetermined direction in a second direction orthogonal to said first direction, at said output terminals, said output terminals being coupled to said antenna drive means input terminals; and

search command generator means coupled to said antenna drive means input terminal for providing search command signals λ

_del and λ

_daz, said directive antenna'"'"'s motion in said first direction being responsive to said signal λ

_del and said directive antenna'"'"'s motion in said second direction being responsive to said signal λ

_daz.

10. The invention according to claims 2 or 3 further comprising:

first switch means having first input means coupled to said frequency discriminator means, second input means coupled to said difference means, and output means, for switchably coupling said output means of said first switch means to said input means of said first switch means;

second switch means having first input means coupled to said range search generator, second input means coupled to said first switch means output means, and output means coupled to said transmitter oscillator drive means for switchably coupling said output means of said second switch means to said input means of said second input means; and

threshold detector means coupled to said discriminator means for comparing said frequency discriminator signal to predetermined threshold signals, and for actuating said first and second switches in the presence of signals greater than said first threshold signal.

11. The invention according to claims 2 or 3 further comprising:

first switch means having first input means coupled to said search command generator and second input means coupled to said angle track demodulator means, and output means coupled to said antenna drive means, for switchably coupling said third switch input means to said third switch output means; and

acquisition detector means coupled to receive said target range bin signals for comparing said target range bin signals to a second predetermined threshold signal, and for actuating said third switch means in the presence of a signal greater than said second threshold signals.

12. The invention according to claims 2 or 3 wherein said range bin means comprises:

a plurality of narrow band filters having substantially contiguous passbands and having input means coupled to receive said beat frequently signal, and output means, for providing a plurality of output signals each of which is indicative of a target in a corresponding range;

a plurality of detector means coupled to said narrow band filters output means for detecting the amplitude of signals received from said narrow band filter and for providing a plurality of detected output signals; and

multiplexer means coupled to said detector means for selecting one of said detected output signals indicative of the presence of said target in said corresponding range and for providing signals representative thereof, and for further selecting detected output signals indicative of ranges adjacent to said target range.

13. The invention according to claim 11 wherein said detector means comprises diodes.

14. The invention according to claims 2 or 3 wherein said frequency discriminator means comprises:

limiter means responsive to said beat frequency signal; and

discriminator circuit means responsive to said limiter means.

15. The apparatus according to claims 2 or 3 further comprising integrator means switchably responsive to said difference means and said frequency discriminator means, and having an output means switchably coupled to said transmitter oscillator drive means.

17. The apparatus of claims 2 or 3 wherein:

said angle track demodulators comprise an azimuth angle demodulator responsive to said target range bin signal for providing azimuth angle error signals Kε

_a and an elevation angle demodulator responsive to said target range bin signal for providing elevation angle error signals Kε

_e ; and

said antenna drive means comprises elevation and azimuth servomotors, coupled to said antenna and responsive to said elevation and azimuth demodulators respectively.

18. The invention according to claims 2 or 3 wherein said transmitter oscillator drive means comprises:

voltage controlled oscillator switchably responsive to said difference means and said range search generator means; and

signal linearizer means having an input coupled to said voltage controlled oscillator means and an output coupled to said transmitter oscillator means.

3. A high frequency, vehicle coupled, target detecting seeker system having twist reflector antenna means coupled to a receiver means comprising:

transmitter oscillator means coupled to said directive antenna means for illumination of targets and background by said directive antenna means, and further coupled to said receiver means for generating therein a beat frequency signal in the presence of said illuminated target or background;

transmitter oscillator drive means having input terminals and output terminals, said output terminals being coupled to said transmitter oscillator for providing transmitter oscillator drive signals at said output terminals responsive to the amplitude of signals applied to said input terminals, the frequency of said transmitter oscillator signals being responsive to said transmitter oscillator drive signals;

a plurality of range bin means coupled to receive said beat frequency signal, each of said range bins being responsive to illuminated objects in substantially contiguous predetermined ranges and for providing output signals from a bin corresponding to the range of said illuminated target, and for further providing signals from bins correspondiing to ranges adjacent to said target range;

difference means having input terminals coupled to receive said signals corresponding to ranges adjacent to said target, for providing in said tracking mode a signal representative of the difference in amplitude of said adjacent range bin signals to said oscillator drive means;

frequency discrimination means having input means coupled to receive said beat frequency signal and having an output means coupled to said transmitter oscillator drive means for providing in said tracking mode, background range tracking signals to said transmitter drive means upon departure of said beat frequency from a predetermined frequency value;

range search generator means switchably coupled to said transmitter oscillator drive means for providing in said search mode range search signals;

antenna drive means having input terminals and being coupled to said directive antenna means, for varying the position of said directive antenna means in space in first and second directions, said first and second directions being orthogonal, in response to signals applied to saiid antenna drive means input terminals;

angle track demodulator means having input terminals coupled to receive said target range bin signal and output terminals, for providing signals Kε

_e representative of the difference between said antenna'"'"'s actual and desired line of sight rate of angular change with respect to a first predetermined reference in said first direction, and signals Kε

_a representative of the difference between said antenna'"'"'s actual and desired line of sight rate of angular change with respect to said first predetermined direction in said second direction at said output terminals, said output terminals being coupled to said antenna drive means input terminals;

search command generator means coupled to said antenna drive means input terminals for providing search command signals λ

_del and λ

_daz, said directive antenna'"'"'s motion in said first direction being responsive to said signal λ

_del and said directive antenna'"'"'s motion in said second direction being responsive to said signal λ

_daz ;

first angle sensor means coupled to said antenna drive means for providing signals β

representative of said antenna drive means angle in said first direction with respect to said first predetermined reference;

second angle sensor means coupled to said antenna drive means for providing signals ψ

representative of said antenna drive means angle in said second direction with respect to said first predetermined reference;

first vehicle rate sensor means coupled to said vehicle for providing signals θ

_p representative of the angular rate of change of said vehicle in a third direction with respect to a second predetermined reference;

second vehicle rate sensor means coupled to said vehicle for providing φ

_R representative of the angular rate of change of said vehicle in a fourth direction orthogonal to said third direction, with respect to said predetermined reference;

third vehicle rate sensor means coupled to said vehicle for providing signals φ

_y representative of the angular rate of change of said vehicle in a fifth direction orthogonal to said third and fourth directions, with respect to said second predetermined reference; and

antenna control means coupled to said antenna drive means and adapted to receive said signals Kε

_e, Kε

_a, θ

_p, φ

_R, θ

_y, β

, ψ

, λ

_del, and λ

_daz for providing signals in said tracking mode for controlling said antenna drive means rate of angualr change β

in said first direction substantially according to the formula;

space="preserve" listing-type="equation">β

=1/2(Kε

.sub.e -θ

.sub.p +2ψ

θ

.sub.R)

and for further providing signals in said tracking mode for controlling said antenna drive means angular rate of change ψ

in said second direction substantially accordiing to the formula;

space="preserve" listing-type="equation">ψ

=1/2(Kε

.sub.a -θ

.sub.y -2β

φ

.sub.R)

and for providing signals in said search mode for controlliing said antenna drive means angular rate of change β

in said first directiion substantially according to the formula;

space="preserve" listing-type="equation">β

=1/2[K(-∫

(θ

.sub.p -2φ

.sub.R ψ

)dt+λ

.sub.del -2β

)-(θ

.sub.p -2φ

.sub.R ψ

)]

and for further providing signals in said search mode for controlling said antenna drive means angular rate of change ψ

in said second direction substantially according to the formula;

space="preserve" listing-type="equation">ψ

=1/2[K(-∫

(φ

.sub.y+ 2β

φ

.sub.R)dt+λ

.sub.daz -2ψ

)-(φ

.sub.y+ 2β

φ

.sub.R)].

9. second switch means having first input means coupled to said second angle amplifier, second input means adapted to receive said signal Kε

_a, and output means coupled to said second rate amplifier for switchably coupling said output means of said second switch means to said input means of said second switch means; and

acquisition detector means responsive to said target range signals and coupled to said first and second switch means for comparing said target range signals to a second predetermined threshold signal, and for actuating said first and second switch means in the presence of a signal greater than said second threshold signal.