Synchronous Control Mathematical Logic in Helicopter Flight Control and Vital Parameters

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.

Synchronous Control Mathematical Logic in Helicopter Flight Control and Vital Parameters Keywords:

control system , information interaction , helicopter , stability