FIELD: transportation.
SUBSTANCE: system of anti-spin control of airplane includes unit of airplane attack current angles detection, unit for setting of critical attack angles of airplane, unit for comparison of current attack angles with critical values, and also facilities for generation of control action. System is equipped with pulse jet engines fixed on airplane fuselage. Facilities include unit for detection of aerodynamic and damping accelerations, unit for detection of values of main and correction force pulses in transverse direction of airplane motion, shaper of signal for connection of pulse jet engines and actuating mechanisms of pulse jet engines. Method for control of airplane is characterised by application of anti-spin control system.
EFFECT: higher safety of airplane piloting.
6 cl, 2 dwg
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Authors
Dates
2009-09-27—Published
2007-09-03—Filed