Applied Physics and Mathematics Annotation << Back
THE DEVELOPMENT OF ALGORITHMS OF DIAGNOSTIC OF EMERGENCY
SITUATIONS, WHICH REQUIRE IMMEDIATE RESCUE SYSTEMS
ACTIVATION DURING TAKOOFF, LANDING, LOW ALTITUDE FLIGHT |
V.I. AKHRAMEEV, G.I. DZHANDZHGAVA, D.V. SHOULEPOV
In the article the brief analysis of fl ight accidents statistics
is given, which confi rms the neccesarity of automation of
emergency crew rescue during take-off , landing, low altitude
fl ight. The emergency situations, which require automatic
command for the pilot to escape, or automatic forced escape,
are found out and divided into groups. The algorithms
of diagnostics of emergency and critical situation, which
require the forced ejection or rescue system activation, are
also developed. Nowadays there are rescue systems for light
aircrafts available at the market, for example, MBEH (Russia),
Junkers Magnum 601 LSA and so on. They can rescue the crew
together with the aircraft (with MTOW less, than 600 kg) at the
speed up to 280 km/h. That gives an opportunity of rescue
automation not only on military airplanes, but also in light civil
aviation.
Key words: fl ight safety, piloting errors, fl ight accident, fl ight accident
statistics, forced emergency escape, emergency rescue,
low-altitude fl ight, crew intellectual support, diagnosis of critical
fl ight modes, voice warning and commands.
Contacts: E-mail: akhrameev_vi@mail.ru, E-mail: rpkb@rpkb.ru, E-mail: dvs04@mail.ru
Pp. 22-40. |
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