FIELD: radio height meters, aircraft engineering.
SUBSTANCE: method includes inserting device marks, determined by distance between antennae mounted on aircraft, methodical errors ΔHM of aircraft flight height change are calculated, caused by operation of device on two antennae, these are inputted during making of device into hard memory, normal methods are used to measure flight height Hni, it is then inputted into memory, from it value of methodical error ΔHMi is taken, on measured height Hni it is subtracted from height Hni and received value H = Hni - ΔHMi is presented to user of height information.
EFFECT: higher precision.
1 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| PULSE RADIO HEIGHT METER | 2004 |
|
RU2258943C1 |
| RECYCLING RADIO ALTIMETER | 2004 |
|
RU2273862C1 |
| METHOD OF MEASURING RELATIVE FLIGHT ALTITUDE OF "AIR-SURFACE" CLASS ROCKETS | 2002 |
|
RU2249830C2 |
| METHOD OF MEASURING FLIGHT ALTITUDE OF AIRCRAFT AT LOW AND ULTRALOW ALTITUDES DURING APPROACH LANDING | 2014 |
|
RU2568293C1 |
| PULSE RADAR ALTIMETER | 2012 |
|
RU2519914C2 |
| METHOD OF REDUCING LOWER BOUNDARY OF LOW ALTITUDE MEASUREMENT TO ZERO AND DESIGN OF COHERENT IMPULSE DOPPLER RADIOALTIMETRE TO THIS END | 2008 |
|
RU2412450C2 |
| RADAR PULSE RE-CIRCULATION RADIO ALTIMETER | 2004 |
|
RU2282211C2 |
| METHOD OF ENHANCING ACCURACY OF BAROMETRIC ALTIMETER WITH THE USE OF SATELLITE POSITION LOCATING SYSTEM | 2006 |
|
RU2316785C1 |
| RADAR METHOD OF DETERMINING FLIGHT ALTITUDE OF AIRCRAFT | 2014 |
|
RU2588105C2 |
| METHOD OF DETERMINING ANGULAR MOTION PARAMETRES OF PILOTLESS AIRCRAFT | 2008 |
|
RU2374609C2 |
