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204results about "Proximity fuzes" patented technology

Passive doppler fuze

A passive proximity fuze. The inventive fuze (10) is adapted to be mounted on a munition (11) and includes a receiver (16) adapted to lock on to a signal transmitted by a target transmitter (12). The receiver (16) detects a Doppler shift in the signal as the munition approaches the target. When a closest point of approach is reached the Doppler shift changes from increasing to decreasing. The inventive fuze (10) includes a mechanism for detecting this change in the Doppler shift and provides a detonation signal in response thereto. In the illustrative embodiment, the receiver (16) is an FM receiver. The mechanism for detecting a change in the Doppler shift may be implemented with discrete analog circuitry or digital circuitry. In an illustrative analog implementation, first and second resistive/capacitive networks (R1C1 and R2C2) are employed to compute a second derivative of the Doppler shift signal output by the receiver (16). This signal is then amplified and thresholded to provide the output detonation signal. In an illustrative digital implementation, the output of the receiver (16) is converted to digital and processed by a digital signal processor (26). The DSP 26 computes the second derivative of the Doppler shift signal output by the receiver (16) in response to a stored program for computing same. The output of the DSP is the detonation signal. Hence, detonation is achieved at the closest point of approach of the munition (11) to the target (12) with an inexpensive passive solution (10).
Owner:RAYTHEON CO

System and method for obtaining precise missile range information for semiactive missile systems

A system (10) for determining the range between a missile (14) and a target (18) adapted for use with a semi-active missile system. The system (10) includes a first circuit (12) for generating a periodic signal (24) that is periodically frequency modulated. A second circuit (16) determines a closing rate at which the missile 14 is approaching the target 18 via the periodic signal 24. A third circuit (16) determines a value containing information corresponding to the range and the closing rate via the periodic signal. A fourth circuit (16) determines the range from the closing rate and the value. In a specific embodiment, the first circuit (12) includes an illumination system (12). The illumination system (12) includes a periodically modulated carrier signal generator (32) that generates the periodic signal (24). The periodically modulated carrier signal generator (32) includes a frequency source, a frequency modulator, and an illumination system computer. The illumination system computer runs software for adjusting the modulation parameters of the frequency modulator. The second, third and fourth circuits (16) are included in a receiver system (16) onboard the missile (14). The receiver system (16) includes a front receiver located near the front of the missile and a rear receiver located near the rear of the missile (14). A receiver system computer runs software that implements the fourth circuit (16). The receiver system (16) includes a local oscillator for providing a reference frequency for the receiver system. The local oscillator derives the reference frequency from the periodic signal provided by the first circuit. In illustrative embodiment, the fourth circuit (16) runs computer software that subtracts the closing rate from the combination of closing rate and range and provides the range in response thereto.
Owner:RAYTHEON CO

Pseudo-random code system-based laser fuze system and target identification method thereof

The invention discloses a pseudo-random code system-based laser fuze system and a target identification method thereof. The laser fuze system adopts a six-quadrant detection scheme, and each pair of detection transceiver systems comprises a pseudo-random code generator, an excitation circuit, a laser, a detector, a signal processing circuit, and transmitting and receiving optical systems; the pseudo-random code generator is used for generating a pseudo-code signal with certain code element width and frequency, the pseudo-code signal is modulated to obtain a pseudo-code pulse signal meeting the requirement of pulse width of the laser, and the pseudo-code pulse signal is excited by the excitation circuit to drive the laser to transmit encoded laser pulse; finally, a laser beam irradiates to a target after being collimated or extended by a transmitting optical system, and the optical energy reflected from the target is received by the receiving optical system; meanwhile, the filtering of a filter and the focusing of the light beam are completed, and after the detector completes the photoelectric conversion and the signal preprocessing of the signal processing circuit, an echo pseudo-random coded signal is obtained after threshold comparison.
Owner:SHANGHAI DIANJI UNIV
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