Impulse radar guidance apparatus and method for use with guided projectiles
First Claim
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1. An impulse radar guided projectile system for guiding a spinning proectile comprising:
- a spinning projectile comprising a receiver for receiving commands, maneuvering means responsive to command signals received by the receiver for causing a terminal maneuver of the spinning projectile, and a reflecting dipole antenna having a switching diode disposed between respective halves of the dipole antenna;
a launcher for launching the spinning projectile at a target; and
tracking means;
for computing a fly-out range for the spinning projectile and a direction at which the maneuvering means is actuated to guide the projectile to the target;
for tracking the rotation of the spinning projectile during projectile'"'"'s flight by radiating a linearly polarized asymmetric waveform at the spinning projectile that comprises a series of repeating pulses having a relatively strong, short, positive electric field pulse followed by a relatively weak, long, negative electric-field baseline;
for processing signals reflected from the dipole antenna to generate signals that are indicative of roll orientation of the spinning projectile, which reflected signals are indicative of the roll orientation of the spinning projectile, whereby a relatively strong signal is reflected from the dipole antenna when the electric field pulse of the asymmetric waveform is aligned along a conduction direction of the diode, a relatively weak signal is reflected when the antenna and diode are aligned orthogonal to the electric field pulse, and a small, non-zero signal is reflected when the diode is aligned anti-parallel to the electric field pulse and the diode is back-biased so that respective halves of the antenna are disconnected; and
for commanding the maneuvering means to deflect the spinning projectile at a specific roll-angle derived from the processed reflected signals to change the flight direction of the spinning projectile so that the spinning projectile is guided at the target.
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Abstract
An impulse radar guidance system and method for use with a spinning projectile. The system and method tracks the flight of the spinning projectile using an all-weather radar or tracker. A linearly polarized asymmetric waveform is transmitted at the projectile that comprises a series of repeating pulses having a relatively strong, short, positive electric field pulse followed by a relatively weak, long, negative electric-field baseline. The projectile contains a dipole antenna having a switching diode disposed between respective halves thereof. The waveform is reflected from the antenna which spins with the projectile and reflects a relatively strong signal when the electric field pulse of the asymmetric waveform is aligned along a conduction direction of the diode, a relatively weak reflected signal when the antenna and diode are aligned orthogonal to the electric field pulse, and a small, non-zero, signal when the diode is aligned anti-parallel to the electric field pulse and the diode is back-biased so that respective halves of the antenna are disconnected. The radar or tracker measures the instantaneous roll angle of the spinning projectile during its flight as a function of the state of the reflected signal. The projectile has a maneuvering device, and a receiver that receives commands that causes the maneuvering device to actuate at one or more specific roll-angles to deflect the flight direction of the projectile at a target.
45 Citations
12 Claims
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1. An impulse radar guided projectile system for guiding a spinning proectile comprising:
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a spinning projectile comprising a receiver for receiving commands, maneuvering means responsive to command signals received by the receiver for causing a terminal maneuver of the spinning projectile, and a reflecting dipole antenna having a switching diode disposed between respective halves of the dipole antenna;
a launcher for launching the spinning projectile at a target; and
tracking means;
for computing a fly-out range for the spinning projectile and a direction at which the maneuvering means is actuated to guide the projectile to the target;
for tracking the rotation of the spinning projectile during projectile'"'"'s flight by radiating a linearly polarized asymmetric waveform at the spinning projectile that comprises a series of repeating pulses having a relatively strong, short, positive electric field pulse followed by a relatively weak, long, negative electric-field baseline;
for processing signals reflected from the dipole antenna to generate signals that are indicative of roll orientation of the spinning projectile, which reflected signals are indicative of the roll orientation of the spinning projectile, whereby a relatively strong signal is reflected from the dipole antenna when the electric field pulse of the asymmetric waveform is aligned along a conduction direction of the diode, a relatively weak signal is reflected when the antenna and diode are aligned orthogonal to the electric field pulse, and a small, non-zero signal is reflected when the diode is aligned anti-parallel to the electric field pulse and the diode is back-biased so that respective halves of the antenna are disconnected; and
for commanding the maneuvering means to deflect the spinning projectile at a specific roll-angle derived from the processed reflected signals to change the flight direction of the spinning projectile so that the spinning projectile is guided at the target. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A method of guiding a spinning guided projectile at a target, said method comprising the steps of:
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launchingia spinning projectile at the target, which projectile comprises a receiver for receiving command signals, maneuvering means responsive to the command signals received by the receiver for causing a terminal maneuver of the spinning projectile toward the target, and a reflecting dipole antenna having a switching diode disposed between respective halves of the dipole antenna;
computing a fly-out range for the spinning projectile and a direction at which the maneuvering means is actuated to guide the projectile to the target;
tracking the rotation of the spinning projectile during the projectile'"'"'s flight by;
radiating a linearly polarized asymmetric waveform at the spinning projectile that comprises a series of repeating pulses having a relatively strong, short, positive electric field pulse followed by a relatively weak, long, negative electric-field baseline;
reflecting a relatively strong reflected signal from the dipole antenna when the electric field pulse of the asymmetric waveform is aligned along a conduction direction of the diode, reflecting a relatively weak reflected signal when the antenna and diode are aligned orthogonal to the electric field pulse, and reflecting a small, non-zero, reflected signal when the diode is aligned anti-parallel to the electric field pulse and the diode is back-biased so that respective halves of the antenna are disconnected;
processing the reflected signals reflected from the dipole antenna to generate signals that are indicative of roll orientation of the spinning projectile, wherein the relatively strong reflected signal is indicative of a predefined angular orientation of the projectile, wherein the relatively weak reflected signal is indicative of an angular orientation that is 180°
opposed to the predefined angular orientation of the projectile, and wherein the small, nonzero, reflected signal is indicative of angular orientations that are orthogonal to the predefined angular orientation of the projectile; and
commanding the maneuvering means to deflect the spinning projectile at a specific roll-angle derived from the processed reflected signals to change the flight direction of the spinning projectile so that the spinning projectile is guided at the target. - View Dependent Claims (12)
synthesizing ultra wideband short pulses from individual spectral components to form an asymmetric waveform;
linearly polarizing the synthesized ultra wideband short pulses; and
radiating the linearly polarized synthesized ultra wideband short pulses.
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Specification
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Current AssigneeRaytheon Company (Rtx Corporation)
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Original AssigneeRaytheon Company (Rtx Corporation)
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InventorsSchneider, Arthur J., Small, James G.
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Primary Examiner(s)Jordan, Charles T.
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Assistant Examiner(s)Wesson, Theresa M.
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Application NumberUS08/940,173Time in Patent Office1,813 DaysField of Search244/3.19, 244/3.16, 244/3.15, 244/3.14, 244/3.13, 244/3.11US Class Current244/3.14CPC Class CodesF41G 7/305 for spin-stabilized missiles
