FIELD: technology and systems for controlling aircrafts from control station, possible use for measuring coordinates (by bank and course) or selection of commands, formed by pulse signal, for example, with time-pulse modulation.
SUBSTANCE: in the method for selection of commands prior to decoding length is extended for each pulse, amplitude of which exceeds value of pass threshold, and fronts of extended pulses are utilized to form low-duration normal pulses, while duration of extended pulses should be less than minimally possible duration between neighboring fronts of adjacent pulses in pulse signal, but greater than time range, during which false pulses can be formed, to extend dynamic range of power alternation of input signal. Insertion into command selection device of serially connected pulse extender and normalizing device expands dynamic range of signal power alternation at device input and simplifies construction of device.
EFFECT: expanded dynamic range of alternation of input signal power, simplified construction of device.
2 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD AND DEVICE FOR COMMAND SEPARATION | 2001 |
|
RU2212761C2 |
| METHOD FOR FORMATION OF MISSILE CONTROL COMMANDS AND MISSILE FOR ITS REALIZATION | 2003 |
|
RU2241949C2 |
| COMBINED CONTROL METHOD OF ROCKET IN BEAM, CONTROL METHOD FOR ITS IMPLEMENTATION, FORMATION METHOD OF N COMMANDS AT CONTROL STATION FOR COMBINED ROCKET CONTROL IN BEAM, EXTRACTION METHOD OF N COMMANDS ON ROCKET FOR COMBINED CONTROL IN BEAM, AND DEVICE FOR ITS IMPLEMENTATION | 2010 |
|
RU2431106C1 |
| MODE OF MEASURING OF COORDINATES AND AN ARRANGEMENT FOR ITS EXECUTION | 2005 |
|
RU2300777C2 |
| METHOD FOR FORMATION OF CONTROL COMMANDS ON ROLL-STABILIZED ROCKET, AND CONTROL SYSTEM OF ROLL-STABILIZED ROCKET | 2004 |
|
RU2280226C1 |
| METHOD AND DEVICE FOR MEASUREMENT OF COORDINATES | 2001 |
|
RU2223514C2 |
| SIGNAL DECODING METHOD AND COORDINATES MEASURING DEVICE IMPLEMENTING THIS METHOD | 2002 |
|
RU2228574C2 |
| METHOD FOR FORMATION OF CONTROL COMMANDS ON MISSILE AND MISSILE CONTROL SYSTEM | 2004 |
|
RU2266513C1 |
| 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 AND DEVICE FOR SIGNAL DECODING | 2004 |
|
RU2280324C1 |
