FIELD: navigational complexes of flying vehicles, multi-mission fighters and helicopters in particular. SUBSTANCE: proposed combined navigational complex includes inertial navigational system, satellite navigational system, navigation computer, navigation information recorder, inertial navigational system error computer, energy-independent storage and first computer of errors to speed components and azimuth angle of gyro-platform of inertial navigational system. Introduced additionally are flying vehicle speed single-beam radar meter, speed radar meter error computer and second computer of errors to speed components and azimuth angle of gyro-platform of inertial navigational system. EFFECT: enhanced accuracy of determination of navigational parameters, noise immunity and resistance to failure. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
FLYING VEHICLE NAVIGATION COMPLEX | 2000 |
|
RU2170410C1 |
FLYING VEHICLE NAVIGATION COMPLEX | 2005 |
|
RU2293950C1 |
COMBINED NAVIGATION SYSTEM | 2003 |
|
RU2229686C1 |
NAVIGATIONAL COMPLEX FOR FLYING VEHICLE | 2003 |
|
RU2230294C1 |
SHIP NAVIGATION SYSTEM | 2011 |
|
RU2478187C2 |
SYSTEM FOR ESTIMATION OF ONBOARD RADAR ACCURACY CHARACTERISTICS | 2006 |
|
RU2314553C1 |
AEROGRAVIMETRIC COMPLEX | 1996 |
|
RU2090911C1 |
INTEGRATED FLIGHT-NAVIGATIONAL COMPLEX OF A FLYING VEHICLE | 2003 |
|
RU2251663C1 |
CONTROL SYSTEM OF UNMANNED AIRCRAFT WITH NAVIGATIONAL COMPLEX | 1994 |
|
RU2046736C1 |
NAVIGATION SYSTEM | 2007 |
|
RU2348011C1 |
Authors
Dates
2004-02-20—Published
2003-03-24—Filed