FIELD: transport.
SUBSTANCE: invention relates to a pilot-navigation systems of a transport aircraft. Digital pilot-navigation system of a transport-aircraft comprising an equipment of current flight navigation parameters for measuring heading, roll, pitch, inertial speeds (IS-1), (IS-2), air speed, pressure altitude (ADS), relative height from the radar altimeter (RA) for determining coordinates by inertial radio systems, a switching unit (SU), a digital-to-analogue converter (DAC), a commands execution unit (CEU), a radio communication system with a receiver-transmitter (RT) to communicate with a control panel at the route initial point (RIP) and a control panel at the route final point (RFP), also additionally includes a satellite navigation system (SNS), a route program unit (RPU), a takeoff-landing unit (TLU), has the first and the second automatic navigators (AN).
EFFECT: technical result is providing unmanned aircraft control together with higher accuracy of the pilot-navigation system and flight safety.
1 cl, 1 dwg
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Authors
Dates
2016-09-20—Published
2015-06-26—Filed