FIELD: rockets control systems.
SUBSTANCE: method includes additional broad-impulse modulation of broad-impulse modulated control signal, during that process load current value is measured, it is compared to values of given thresholds of enabling and disabling load, and on basis of results of comparing value of additional broad-impulse modulation coefficient is set, by which nominal load current is set. Device has power source, broad-impulse control signal modulation forming means, load, electronic key, current sensor, two-threshold device for comparing to set unit of enabling and disabling thresholds of load and match circuit.
EFFECT: higher precision of regulation of nominal load current with excluded instability due to automatic regulation of additional broad-impulse modulation coefficient.
5 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR ADJUSTMENT OF RATED CURRENT CONTROL OF AIRCRAFT DRIVE OPERATING SOLENOID AND DEVICE FOR ITS IMPLEMENTATION | 2015 |
|
RU2606213C1 |
METHOD FOR FORMATION OF MISSILE CONTROL COMMANDS AND MISSILE FOR ITS REALIZATION | 2003 |
|
RU2241949C2 |
METHOD AND DEVICE FOR MODULATING PULSED OPTICAL RADIATION (ALTERNATIVES) | 2005 |
|
RU2300841C1 |
METHOD AND DEVICE FOR CODING ELECTROMAGNETIC RADIATION | 2002 |
|
RU2234795C2 |
METHOD FOR FORMATION OF CONTROL COMMANDS ON ROLL-STABILIZED ROCKET, AND CONTROL SYSTEM OF ROLL-STABILIZED ROCKET | 2004 |
|
RU2280226C1 |
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 |
|
RU2283466C1 |
CLASS D AMPLIFIER CHANNEL PULSE WIDTH MODULATOR | 2022 |
|
RU2796945C1 |
SIGNAL DECODING METHOD AND COORDINATES MEASURING DEVICE IMPLEMENTING THIS METHOD | 2002 |
|
RU2228574C2 |
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 |
|
RU2282129C1 |
METHOD OF INTRODUCING ROCKETS INTO ZONE OF CONTROL, ROTATING ALONG ANGLE OF LIST, AND ROCKET SYSTEMS | 2007 |
|
RU2362107C2 |
Authors
Dates
2004-08-27—Published
2002-11-04—Filed