FIELD: radio engineering, communication.
SUBSTANCE: adjustment shield simulates forward radio signals and radio signals specularly reflected from the earth, propagating from a missile and a target to a final homing area. The adjustment shield is located in the far zone of a radio direction-finding antenna and comprises laser and infrared emitters. To simulate signals from a missile transponder and signals reflected from a target, the shield is provided with a radio pulse generator with a frequency synthesiser.
EFFECT: high accuracy of adjustment.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF DETERMINING SYSTEMATIC ERRORS IN LOCATING MISSILE AND TARGET USING MONOPULSE SYSTEM | 2010 |
|
RU2454677C1 |
ADJUSTING TOWER | 2009 |
|
RU2406066C1 |
METHOD OF IDENTIFICATION OF INFORMATION MEANS OF AIR-DEFENSE FIGHTING MACHINE AND DEVICE FOR IDENTIFICATION OF INFORMATION MEANS THEREOF | 2017 |
|
RU2670242C1 |
ADJUSTMENT DEVICE | 2018 |
|
RU2705790C1 |
METHOD FOR GUIDING ROCKET MISSILE AND OPTOELECTRONIC COMMAND GUIDANCE SYSTEM | 2005 |
|
RU2288424C1 |
MISSILE GUIDANCE DEVICE | 1996 |
|
RU2100746C1 |
ANTIAIRCRAFT ROCKET AND GUN COMPLEX | 1998 |
|
RU2131577C1 |
OPTOELECTRONIC SYSTEM FOR AIR DEFENCE MISSILE SYSTEM | 2010 |
|
RU2433370C1 |
OPTOELECTRONIC SYSTEM OF ANTIAIRCRAFT MISSILE COMPLEX | 1999 |
|
RU2165582C2 |
METHOD FOR TWO-DIMENSIONAL MONOPULSE DIRECTION FINDING OF RADIO EMISSION SOURCES | 2019 |
|
RU2696095C1 |
Authors
Dates
2015-04-20—Published
2014-04-29—Filed