FIELD: armament, applicable in system of artillery, tank and anti-tank armament, as well as of small-sized guided missiles of anti-aircraft systems.
SUBSTANCE: the single-channel rolling missile uses a relay control actuator and provides for proportionality of the values of the control commands and control surface deflections of the single-channel relay control actuator in each plane by the original control signal in the co-ordinate measuring system. The signal formed by the device is supplied to the single-channel relay three-position control actuator that follows this signal, i.e. reverses the control surfaces in compliance with variation of its sign. The rolling missile demodulates the deflection of the control surfaces, as a result of which, control moment proportional to the respective error signals in the measuring co-ordinate system are produced in the vertical and horizontal planes.
EFFECT: enhanced accuracy of guidance.
8 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR FORMATION OF RELAY CONTROL SIGNALS OF SPIN-STABILIZED MISSILE | 2000 |
|
RU2184921C2 |
| ROTATING MISSILE GUIDANCE WITH CONTROL SURFACE RELAY DRIVE AND SYSTEM TO THIS END | 2008 |
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| METHOD OF GUIDANCE OF SPINNING MISSILE WITH RELAY DRIVE OF STEERING BODY AND SYSTEM OF ITS IMPLEMENTATION | 2013 |
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RU2532993C1 |
| METHOD FOR GUIDANCE OF SPIN-STABILIZED MISSILE WITH RELAY CONTROL ACTUATOR AND SYSTEM FOR ITS REALIZATION | 2005 |
|
RU2310151C2 |
| METHOD TO GENERATE CONTROL INSTRUCTION FOR SPINNING TWO-CHANNEL ROCKET AND DEVICE TO THIS END | 2008 |
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RU2373479C1 |
| METHOD OF SPINNING ROCKET GUIDANCE AND SYSTEM TO THIS END | 2011 |
|
RU2486428C1 |
| METHOD OF COMBINED GUIDANCE OF SMALL-SIZED MISSILE WITH SEPARABLE PROPULSION SYSTEM AND GUIDANCE SYSTEM FOR ITS IMPLEMENTATION | 2014 |
|
RU2569046C1 |
| METHOD OF FORMING CONTROL INSTRUCTION TO SINGLE-CHANNEL MISSILE SPINNING IN ROLL ANGLE AND DEVICE TO THIS EFFECT (VERSIONS) | 2011 |
|
RU2473864C1 |
| DEVICE FOR FORMATION OF COMMANDS TO CONTROL A ROCKET ROTATING AROUND ITS LONGITUDINAL AXIS | 2002 |
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RU2235969C1 |
| METHOD FOR FORMATION OF MISSILE CONTROL COMMANDS AND MISSILE FOR ITS REALIZATION | 2003 |
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RU2241949C2 |
