FIELD: armament, in particular, rocketry, roll-stabilized rockets.
SUBSTANCE: a linearized signal is formed on the rocket from the roll signal, which with regard to the rocket roll angle is compared with the decoded values of the command messages respectively in heading and pitching, rocket control commands are formed in the form of a width-modulated signal as a result of comparison. The swing value of the linearized signal is independent of the roll signal duration and is changed inversely proportionally to the required values of the control commands. Introduction of an OR exclusive logic circuit, relay element and a programming device in the rocket control system has enhanced the accuracy of formation of width-modulated control commands.
EFFECT: enhanced accuracy of formation of width-modulated signals.
2 cl, 4 dwg
| Title |
Year |
Author |
Number |
| METHOD FOR FORMATION OF CONTROL COMMANDS ON SPIN-STABILIZED ROCKET, ROCKET CONTROL SYSTEM, METHOD FOR FORMATION OF LINEARIZED SIGNAL AND SIGNAL LINEARIZER FOR ITS REALIZATION |
2004 |
- Dudka Vjacheslav Dmitrievich
- Nazarov Jurij Mikhajlovich
- Zemlevskij Valerij Nikolaevich
- Morozov Vladimir Ivanovich
|
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2007 |
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|
RU2362107C2 |
| METHOD FOR FORMING OF CONTROL COMMANDS ON SPIN-STABILIZED MISSILE, SPIN-STABILIZED MISSILE, METHOD FOR FORMING OF DOUBLE-SIDEBAND LINEARIZED SIGNAL AND REVERSIBLE SIGNAL LINEARIZER |
2005 |
- Dudka Vjacheslav Dmitrievich
- Zemlevskij Valerij Nikolaevich
- Morozov Vladimir Ivanovich
- Nazarov Jurij Mikhajlovich
|
RU2283466C1 |
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2007 |
- Stepanichev Igor' Veniaminovich
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|
RU2351875C2 |
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2007 |
- Nazarov Jurij Mikhajlovich
- Tjurin Vladimir Fedorovich
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|
RU2362108C2 |
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2011 |
- Gusev Andrej Viktorovich
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- Ovsenev Sergej Sergeevich
- Tarasov Viktor Ivanovich
|
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2012 |
- Gusev Andrej Viktorovich
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|
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| METHOD FOR CORRECTION OF COMMAND SIGNAL ON SPIN-STABILIZED MISSILE AND MISSILE GUIDANCE SYSTEM |
2004 |
- Dudka Vjacheslav Dmitrievich
- Zemlevskij Valerij Nikolaevich
- Morozov Vladimir Ivanovich
- Nazarov Jurij Mikhajlovich
|
RU2280233C1 |
| METHOD OF LINEARISED SIGNAL SHAPING ON MISSILE ROTATING BY BANK ANGLE SIGNAL LINEARISER SWITCHABLE SIGNAL LINEARISER INTEGRATION METHOD FOR LINEARISED SIGNAL SHAPING AND DIGITAL INTEGRATOR FOR ITS IMPLEMENTATION |
2014 |
- Dronov Evgenij Anatol'Evich
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|
RU2549231C1 |
| METHOD FOR CORRECTION OF COMMAND SIGNAL OF MISSILE SPINNING IN BANK ANGLE, AND MISSILE GUIDANCE SYSTEM FOR ITS REALIZATION |
2004 |
- Dudka V.D.
- Nazarov Ju.M.
- Zemlevskij V.N.
- Morozov V.I.
|
RU2257523C1 |
