FIELD: instrument making.
SUBSTANCE: system comprises a primary detection circuit, which includes at least one measurement channel. At the same time the specified measurement channel comprises the following: a device to measure static air pressure; a device to measure sideslip angle of an aircraft; a device to measure dynamic pressure, common temperature and angle of aircraft attack; a device of data processing made as capable of detecting anemobaroclinometric parameters on the basis of measurements of static pressure, sideslip angle, dynamic pressure, common temperature and attack angle; at least one laser anemometer (50) to measure at least one parameter of actual speed of the aircraft.
EFFECT: reliability improvement.
6 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD AND DEVICE FOR CALCULATING CURRENT VALUE OF ANGULAR ATTACKS AND GLIDING OF AERIAL VEHICLE | 2016 |
|
RU2663315C2 |
| SYSTEM OF AERONAUTICAL DATA | 1996 |
|
RU2159443C2 |
| METHOD OF AIRFOIL ACTIVE DEFORMATION | 2009 |
|
RU2485013C2 |
| SYSTEM AND METHOD FOR ESTIMATING AIRSPEED OF AIRCRAFT BASED ON MODEL OF WEATHER DATA ACCUMULATION | 2018 |
|
RU2755843C2 |
| LABEL SENSOR FOR AERODYNAMIC ANGLE AND TRUE AIR SPEED | 2014 |
|
RU2580208C1 |
| METHOD OF CHECKING OF FLIGHT VEHICLE AEROMETRIC PARAMETERS METER AND DEVICE FOR ITS REALIZATION | 1993 |
|
RU2079142C1 |
| LABEL SENSOR FOR AERODYNAMIC ANGLE AND TRUE AIR SPEED | 2014 |
|
RU2585126C1 |
| SYSTEM AND METHOD FOR DETECTING ERRONEOUS PRESSURE MEASUREMENTS IN AIR SIGNAL SYSTEM WITH NON-PROTRUDING PRESSURE RECEIVERS USING PRESSURE DIAGRAMS BETWEEN ADJACENT PRESSURE SAMPLING HOLES | 2019 |
|
RU2771090C1 |
| MODE OF DEFINITION OF AIR-SPEED PARAMETERS OF THE FLIGHT OF FLYING VEHICLES | 2006 |
|
RU2314541C1 |
| SYSTEM AND METHOD FOR ESTIMATING AIRSPEED OF AIRCRAFT BASED ON DRAG MODEL | 2018 |
|
RU2756243C2 |
