FIELD: aircraft systems for control, navigation and detection of targets, guidance and aiming. SUBSTANCE: proposed system includes navigation system, satellite navigation system, radar station, first and second multi-functional indicators, windshield indicator, five on-board computers, navigation information signal multiplexer, reserve mode signal shaper, digital computer, mains multiplexer, tele-signal multiplexer, symbology generator inertial attitude-and-heading reference system unit, electronic short-range navigational system, radio altimeter, video information recorder, radio station and line receiver. EFFECT: extended functional capabilities; enhanced efficiency. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE NAVIGATIONAL COMPLEX | 2000 |
|
RU2170409C1 |
| INDICATION SYSTEM OF AIRCRAFT | 2001 |
|
RU2206872C2 |
| NAVIGATION AND ELECTRONIC DISPLAY COMPLEX | 2003 |
|
RU2215995C1 |
| MULTIFUNCTIONAL ABOARD INDICATOR | 2000 |
|
RU2162204C1 |
| FLYING VEHICLE NAVIGATION COMPLEX | 2000 |
|
RU2170410C1 |
| COMBINED NAVIGATION SYSTEM | 2003 |
|
RU2229686C1 |
| NAVIGATIONAL COMPLEX FOR FLYING VEHICLE | 2003 |
|
RU2230294C1 |
| COMBINED NAVIGATIONAL COMPLEX OF FLYING VEHICLE | 2003 |
|
RU2224220C1 |
| FLYING VEHICLE NAVIGATION COMPLEX | 2005 |
|
RU2293950C1 |
| HELICOPTER ONBOARD HARDWARE COMPLEX | 2012 |
|
RU2520174C2 |
Authors
Dates
2003-11-20—Published
2002-10-17—Filed