FIELD: aircraft pilotage and navigational information systems. SUBSTANCE: proposed complex includes first gyro horizon, second gyro horizon, speed and drift angle Doppler sensor, g-load direction sensor, radio altimeter, gyro-magnetic compass, compass system, automatic radio compass of decimeter range, switch, input-output unit, multi-functional computer, satellite navigation system, first multi-functional indicator, second multi-functional indicator, air signal system, amplifier- splitter and switchboard. EFFECT: enhanced accuracy ; failure resistance; enhanced informative capacity. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
FLYING VEHICLE NAVIGATIONAL COMPLEX | 2000 |
|
RU2170409C1 |
NAVIGATIONAL COMPLEX FOR FLYING VEHICLE | 2003 |
|
RU2230294C1 |
FLYING VEHICLE NAVIGATION COMPLEX | 2000 |
|
RU2170410C1 |
INDICATION SYSTEM OF AIRCRAFT | 2001 |
|
RU2206872C2 |
AIRCRAFT ARMAMENT COMPLEX CONTROL SYSTEM | 2002 |
|
RU2216484C1 |
COMBINED NAVIGATION SYSTEM | 2003 |
|
RU2229686C1 |
MULTIFUNCTIONAL ABOARD INDICATOR | 2000 |
|
RU2162204C1 |
FLYING VEHICLE NAVIGATION COMPLEX | 2005 |
|
RU2293950C1 |
HELICOPTER ON-BOARD EQUIPMENT SET | 2016 |
|
RU2652344C1 |
COMBINED NAVIGATIONAL COMPLEX OF FLYING VEHICLE | 2003 |
|
RU2224220C1 |
Authors
Dates
2003-11-10—Published
2003-02-17—Filed