FIELD: aviation. SUBSTANCE: airfield lighting system model for landing training has N optical channels of various spectral ranges with parallel optical axes, each formed by reflector, radiation source incorporating power controller, light filter, lens, and hood all mounted in tandem and secured on platform; some of radiation sources are of pulse type and remaining ones are continuous-running; in addition, it is provided with range finder connected to visibility range category setter and landing inhibiting indicator, photometer, N light source brightness calculators, N meteorological visibility range metering units for each spectral range, atmosphere scattering coefficient meter (scatterometer), sea brightness coefficient meter (hydrophotometer), atmosphere turbulence meter, color comparator, spectrum analyzer, square-root extraction unit, semi-transparent reflectors, and servo drives. Platform is provided with drives coupled with ship's roll and trim setting elements. EFFECT: improved design. 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SHIP'S DECK LANDING TRAINER | 1991 |
|
SU1798988A1 |
| SHIPBOARD OPTICAL LANDING SYSTEM FOR FLYING VEHICLES | 1993 |
|
RU2083443C1 |
| SYSTEM OF AUTOMATIC CONTROL OF ARRESTING HOOK AND ENGINE IN LANDING OF FLYING VEHICLE ON SHIP'S DECK | 1996 |
|
RU2119440C1 |
| FLIGHT SIMULATION COMPLEX FOR INVESTIGATION OF LANDING SYSTEMS OF SHIP-BASED FLYING VEHICLES | 1991 |
|
RU2042583C1 |
| FLYING VEHICLE ARRESTER HOOK CONTROL DEVICE | 1993 |
|
RU2067951C1 |
| VISIBILITY SIMULATOR OF COMPLEX METEOROLOGICAL CONDITIONS | 1991 |
|
RU2056646C1 |
| FLYING VEHICLE SPEED CONTROL SYSTEM FOR CONTROL OF SPEED DURING DECK LANDING | 1995 |
|
RU2129971C1 |
| DEVICE FOR SIMULATION OF VISUAL ORIENTATION OF PILOT | 1997 |
|
RU2128860C1 |
| METHOD OF MEASURING CHARACTERISTICS OF TRANSPORT VEHICLE AIR WAKE | 1993 |
|
RU2088487C1 |
| PULSE PHOTOMETER | 1997 |
|
RU2116633C1 |
