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Design of a variable rolling speed aircraft based on ATmega16 attitude controller

  • 2013-09-20
  • 174.54KB
  • Points it Requires : 1

Owing to the effect of crosswind, initial disturbance and the deviation of engine parameters.etc in the initial aviation, variable rolling velocity aerocraft will produce attitude angle deviation in the ideal orientations.This paper adopts AVR microcontroller atmega16 and relevant signal process circuit to design the attitude controller and take the method of frequency discrimination and amplitude discrimination to process attitude angle deviation of aerocraft. Accordingly, it amends attitude angle deviation of aerocraft effect and implements the self-adapting attitude control of aerocraft’s rolling velocity.Keywords: Rolling Velocity, Aerocraft, Attitude Controller

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