Synchronous Control Mathematical Logic in Helicopter Flight Control and Vital Parameters

Farshid Bazmi¹ Afsaneh Khaghaniazar² Hadi kavousi³ Negin Loghmani⁴ Saeid Keshtkar Garousi⁵

1) PhD, Aerospace Engineering,
2) MSc, Mathematics and Computer Science,
3) BSc, Electrical Engineering,
4) MSc, Computer Engineering,
5) MSc, Mathematics and Computer Science,

IOI Code : XAGA-DBDKH
Publication : 4th.International Conference on Researches in Science & Engineering & International Congress on Civil, Architecture and Urbanism in Asia(4icrsie.com)
Abstract :
    The main and tail rotors of helicopter and engine control system in which, computers are linked to exchange performance data to control engines and rotors, work together to improve flight performance. This article is about a main rotor synchronous control system, tail rotor, engine gearbox, and main rotor, a set of pilot control systems, active helicopter control computer, engine control computer, main rotor operators and tail rotor which the defects of previous control systems are reduced or eliminated in general. The precision level of this engine control system in maintaining turbine torque is very important in the desired range, especially when using multiple engines simultaneously. The complete response of the system governing the engine is important in preventing excessive transmission of changes in the rotor speed, and special tools are needed to ensure the present torsional stability.

Keywords : control system information interaction helicopter stability