FIELD: physics; navigation.
SUBSTANCE: invention relates to instrument making and can be used in aircraft navigation systems. The technical outcome is widening of functional capabilities. To achieve this outcome, the device includes a unit of initial information sensors, an analogue-to-digital converter (ADC), a computer, an alternating voltage source, a decoder, conversion channels, a register, a digital-to-analogue converter (DAC) and a power amplifier.
EFFECT: device enables converting digital information on the current values of angles of position of the aircraft to analogue signals, proportional to their sine or cosine.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SHAFT TURN ANGLE-TO-DIGITAL CONVERTER | 0 |
|
SU1312737A1 |
| DEVICE TO INTEGRATE STANDBY INSTRUMENT INTEGRATED SYSTEM ORIENTATION UNIT WITH AIRCRAFT INSTRUMENTATION COMPLEX | 2013 |
|
RU2537514C1 |
| DEVICE FOR MEASUREMENT OF ROTARY TRANSFORMER STATIC ERROR | 2008 |
|
RU2362178C1 |
| SHAFT ANGLE OF TURN CONVERTER | 0 |
|
SU1334373A2 |
| METHOD AND DEVICE FOR CONVERTING SHAFT ANGLE-OF-ROTATION INTO CODE | 0 |
|
SU1713103A1 |
| DIGITAL-TO-SHAFT TURN ANGLE CONVERTER | 0 |
|
SU1311030A1 |
| REVERSIBLE COORDINATE CONVERTER | 0 |
|
SU1035617A1 |
| 0 |
|
SU1778766A1 | |
| DIGITAL ANGLE CONVERTER | 2013 |
|
RU2541856C2 |
| MULTICHANNEL TURN ANGLE DIGITIZER | 0 |
|
SU1462478A2 |
