FIELD: armament, in particular, rocketry, applicable in development of missile systems, for example, with carriers on the ground, in which beam riding guidance systems are used.
SUBSTANCE: electromagnetic radiation from the control point is transformed to electric signals of the missile co-ordinates in yaw and pitching, missile control commands in yaw and pitching are formed from the co-ordinate electric signals, the magnitude of the missile co-ordinate is integrated in yaw, then the magnitude of the electric signal co-ordinate in yaw is summed up with its integrated magnitude, and the missile yaw control command is formed from the summary magnitude.
EFFECT: introduction of an adder, integrator and an integrator switching unit in the missile guidance system in the yaw channel has enhanced the accuracy of missile guidance in the yaw channel. 2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR CONTROL OF MISSILE AND MISSILE GUIDANCE SYSTEM FOR ITS REALIZATION | 2003 |
|
RU2241950C1 |
METHOD FOR CONTROL OF MISSILE AND MISSILE GUIDANCE SYSTEM FOR ITS REALIZATION | 2003 |
|
RU2241951C1 |
METHOD FOR ROCKET CONTROL AND ROCKET GUIDANCE SYSTEM FOR ITS REALIZATION | 2005 |
|
RU2295691C1 |
METHOD FOR MISSILE CONTROL (MODIFICATIONS) AND MISSILE CONTROL SYSTEM FOR ITS REALIZATION (MODIFICATIONS) | 2005 |
|
RU2291384C1 |
METHOD FOR ENTRY OF MISSILE INTO BEAM AREA AND COMPLEX OF MISSILE TELECONTROLLED IN BEAM FOR ITS REALIZATION (MODIFICATIONS) | 2003 |
|
RU2257522C1 |
COMBINED BEAM CONTROL METHOD AND MISSILE CONTROL SYSTEM FOR ITS IMPLEMENTATION | 2009 |
|
RU2421680C2 |
METHOD FOR CORRECTION OF COMMAND SIGNAL ON SPIN-STABILIZED MISSILE AND MISSILE GUIDANCE SYSTEM | 2004 |
|
RU2280233C1 |
METHOD FOR CORRECTION OF COMMAND SIGNAL OF MISSILE SPINNING IN BANK ANGLE, AND MISSILE GUIDANCE SYSTEM FOR ITS REALIZATION | 2004 |
|
RU2257523C1 |
METHOD FOR MONITORING OF MISSILE TELECONTROL BEAM SYSTEM AND SYSTEM FOR ITS REALIZATION | 2003 |
|
RU2257526C1 |
METHOD FOR GUIDANCE OF MISSILE TELEORIENTED IN MISSILE BEAM AND MISSILE SYSTEM FOR ITS REALIZATION | 2004 |
|
RU2266509C1 |
Authors
Dates
2006-12-10—Published
2005-05-03—Filed