Guide apparatus radar pulse and method of use with guided projectiles.

摘要

Guidance System RADAR IMPULSE (10) and method (30) for use with a projectile GIRO (11). SYSTEM AND PROCEDURE FOLLOWED THE FLIGHT OF A MISSILE RADAR TURNING USING ALL TIME (14) or a tracking device (14). A waveform asymmetrical linearly polarized (21) IS TRANSMITTED TO MISSILE COMPRISING A BUT SERIES IMPULSE REPEATED (22) HAVING AN IMPULSE ELECTRIC FIELD POSITIVE BRIEF relatively strong (23) FOLLOWED BY A LINE BASE ELECTRIC FIELD (24 ) long lasting and relatively weak. The missile COMPRISING A BIPOLE antenna (26) with a diode switch (27) disposed between SAME RESPECTIVE HALVES. WAVEFORM IS REFLECTED BY AERIAL ROTATING WITH MISSILE AND REFLECTS A relatively strong signal when the pulse electric field WAVEFORM ASIMETRICA is aligned along a direction of the diode, A SIGN REFLECTED RELATIVELY WEAK WHEN ANTENAY DIODE are aligned orthogonally MOMENTUM OF ELECTRIC FIELD AND A SMALL SIGNAL nonzero when the diode is aligned antiparallel WITH MOMENTUM OF ELECTRIC FIELD AND THE DIODE IS BACK BIAS SO THE HALVES RESPECTIVE ANTENNA ARE DISCONNECTED. O RADAR TRACKING DEVICE MEASURING THE ROTATION ANGLE ROTATING INSTANTANEO Projectile, DURING FLIGHT depending on the state of the reflected signal. THE MISSILE HAS A handler (16) and a receiver (15) that receives commands DOING TO OPERATE Switchgear IN ONE OR MORE SPECIFIC TO DIVERT ANGULOS flight direction Projectile ON A WHITE.