| 摘要 |
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 |
