FIELD: weapons and ammunition.
SUBSTANCE: proposed homing head comprises gyro coordinator that includes four-site radiation receiver and control windings, four processing channels, adder, timer, two circuits of sum-and-subtract processing, four OR elements, eight gates and power amplifier. Each processing channel comprises comparator, amplifier and peal detector connected in series, and counter and trigger connected in series. Output of four-site radiation receiver are connected with first inputs of processing channels. Adder inputs are connected with first outputs of processing channels. Timer output is connected with processing channel inputs. Outputs of power amplifier unit are connected by homing head outputs with control windings.
EFFECT: higher reliability in severe operating conditions caused by high load in firing and vibration acceleration in guidance.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LASER SEMIACTIVE SELF-HOMING HEAD | 2011 |
|
RU2476815C1 |
| LASER SEMIACTIVE HOMING HEAD | 2011 |
|
RU2473866C1 |
| LASER SEMIACTIVE HOMING EYE | 2010 |
|
RU2439477C1 |
| OPTICAL POLARIZATION HOMING HEAD WITH SINGLE-ELEMENT INFRARED RADIATION RECEIVER | 2023 |
|
RU2825219C1 |
| AIRBORNE COMPLEX OF CONTROLLING ADJUSTABLE AERIAL BOMB WITH LASER FEATHERED HOMING HEAD, FULFILLED ACCORDING TO THE SCHEME DUCK | 2003 |
|
RU2251656C1 |
| COMBINED MULTI-CHANNEL HOMING HEAD | 2017 |
|
RU2693028C2 |
| GUIDED MISSILE GUIDANCE SYSTEM | 2002 |
|
RU2224972C2 |
| SMALL-SIZE ANTI-AIRCRAFT GUIDED MISSILE | 2018 |
|
RU2694932C1 |
| ROTATING ALONG THE ROLL ANGLE WITH DIRECTION GYROSCOPE TO THE TARGET ACQUISITION ZONE BY THE HOMING HEAD ROCKET OUTPUTTING METHOD AND SYSTEM FOR ITS IMPLEMENTATION | 2017 |
|
RU2659622C1 |
| OPTOELECTRONIC MULTI-CHANNEL HOMING HEAD | 2020 |
|
RU2756170C1 |
