FIELD: weapons and ammunition.
SUBSTANCE: projectile includes electronic control equipment, control members made in the form of aerodynamic rudders, and sensing elements of projectile deviation from the specified trajectory, which are arranged on the basis of two micromechanical gyroscopes (MMG) arranged on two mutually perpendicular boards with radio elements installed on them and providing alignment of MMG signals supplied to electronic control equipment, with its own signals which are supplied to control members. Boards are fixed on common base installed perpendicular to longitudinal projectile axis X so that sensitive axes of MMG are perpendicular to each other and aligned with the corresponding transverse Y and Z axes of the projectile; at that, the base is developed in the projectile rotation direction relative to aerodynamic rudders through the angle the value of which is equivalent to the command shaping time for control members.
EFFECT: improving accuracy and enlarging the firing distance of artillery projectiles.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SMALL-SIZED GUIDED SPINNING MISSILE | 2014 |
|
RU2561319C1 |
| GUIDED JET PROJECTILE | 2012 |
|
RU2502042C1 |
| GUIDED SPIN-STABILIZED PROJECTILE | 2002 |
|
RU2231745C2 |
| METHOD OF CONTROLLING AND STABILISING MOBILE CARRIER, INTEGRATED SYSTEM, DEVICE FOR TURNING ANTENNA REFLECTOR IN TWO MUTUALLY-PERPENDICULAR PLANES AND DEVICE FOR ACTUATING DIFFERENTIAL AERODYNAMIC CONTROLLERS FOR REALISING SAID METHOD | 2009 |
|
RU2423658C2 |
| METHOD OF LONG-RANGE TARGET CAPTURE OF ZONE MISSILE HOMING HEAD AND LONG MISSILE GUIDANCE SYSTEM | 2015 |
|
RU2583347C1 |
| PRINCIPLE OF OPTIC BEAM GUIDANCE OF MISSILE LAUNCHING FROM MOBILE CARRIER | 2011 |
|
RU2498192C2 |
| 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 |
| METHOD OF COMBINED GUIDANCE OF SMALL-SIZED MISSILE WITH SEPARABLE PROPULSION SYSTEM AND GUIDANCE SYSTEM FOR ITS IMPLEMENTATION | 2014 |
|
RU2569046C1 |
| METHOD OF STABILISING ANGULAR POSITION OF ROLL-REVOLVING CONTROLLED ARTILLERY PROJECTILE LENGTHWISE AXIS | 2008 |
|
RU2401981C2 |
| METHOD FOR DETERMINATION OF AERODYNAMIC CHARACTERISTICS OF GUIDED MISSILE IN FLIGHT, METHOD FOR DETERMINATION OF ANGLE OF ATTACK OF MISSILE IN FLIGHT, METHOD FOR DETERMINATION OF MISSILE ATTITUDE AND DEVICES FOR THEIR REALIZATION | 2002 |
|
RU2218550C2 |
