ON-BOARD INTEGRATED CREW SUPPORT INFORMATION SYSTEM AND COGNITIVE FORMAT OF PRESENTING FLIGHT INFORMATION AT TAKE-OFF PHASE OF MULTI-ENGINE AIRCRAFT Russian patent published in 2015 - IPC B64D43/00 G01C21/00 G01C23/00 G05D1/00 

FIELD: physics, computer engineering.

SUBSTANCE: group of inventions relates to self-contained digital integrated systems of on-board equipment of multi-engine aircraft. The on-board information support system comprises a take-off dynamics module, an altitude-speed and meteorological parameter module, a flight characteristics module, an aerodynamics module, an engine thrust module, an aerodrome database module and a global database of the topography of the underlying surface EGPWS of high precision in 3D format and minimum safe altitude, an analysis and decision-making module and other modules. The disclosed cognitive format of presenting information on a flight display includes a synthesized display of the runway with an axial line, the runway threshold, display of the boundaries of maximum allowed lateral deviation of aircraft take-off run and other vital displays. The flight display, on the background of the windscreen, further displays commands to raise the nose wheel, take-off, accelerate the aircraft to safe climbing speeds and commands to maintain an optimum pitch angle at the airborne part of the take-off distance, as well as commands to turn and emergency climb to prevent collision with the underlying surface and manmade obstacles. The formats of said parameters are displayed using principles of activating visual perception of information in information support of the crew in cognitive operations of the crew using principles of artificial intelligence, completeness of information presentation, relevancy and interactivity.

EFFECT: easier control of aircraft and safer flights.

20 cl, 10 dwg, 3 tbl