FIELD: physics.
SUBSTANCE: system includes two radio beacons, two radio compasses and a computer. The radio beacons are placed at the beginning of the landing strip on the left side and the right side of the axis of the landing strip at equal distances. The radio beacons operate each at its own frequency. The radio compasses are installed on the aircraft and are tuned each to the frequency of its own radio beacon. Based on the base direction between the radio beacons and the difference in angle values, the computer of the system determines the direction and distance to the beginning of the landing strip with display of the location of the beginning of the landing strip on a display screen.
EFFECT: safer aircraft landing on a landing strip.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF LANDING APPROACH OF FLYING VEHICLE AND SYSTEM FOR REALIZATION OF THIS METHOD | 1999 |
|
RU2156720C1 |
| METHOD OF AIRCRAFT EMERGENT LANDING APPROACH (VERSIONS) | 2012 |
|
RU2509684C2 |
| METHOD OF AIRCRAFT CONTROL IN LANDING APPROACH | 2011 |
|
RU2478523C2 |
| LIGHT WARNING SYSTEM FOR CATEGORICAL AIRFIELDS AND LIGHT FOR THIS SYSTEM | 1999 |
|
RU2193508C2 |
| AIRFIELD LIGHT WARNING SYSTEM | 1999 |
|
RU2191143C2 |
| METHOD OF VERTICAL LANDING ON UNBUTTONED AIRFIELDS | 2008 |
|
RU2375263C1 |
| METHOD OF VISUAL LANDING AND KIRILLOV'S DEVICE TO SUPPORT AIRCRAFT TAKEOFF OR LANDING | 2011 |
|
RU2475424C1 |
| THREE-DIMENSIONAL LATERAL DEVIATION DISPLAY | 1996 |
|
RU2173660C2 |
| WAY OF LANDING APPROACH | 2008 |
|
RU2364943C1 |
| RADIO BEACON TO ENSURE APPROACH AND LANDING OF HELICOPTERS ON LIMITED LANDING GROUND IN ABSENCE OF GROUND VISIBILITY | 1993 |
|
RU2081428C1 |
