Synthesis of control laws of a pitch channel ofthe autopilot

Authors

  • Valeriy Ivanovich Petunin

Keywords:

Автопилот; угол тангажа; закон управления; передаточные числа; система автоматического управления; статическая система; астатическая система; передаточная функция; переходный процесс

Abstract

The control laws of autopilots taking into account features of dynamics of an airplane on pitch angle are received. These laws allow to ensure the given quality of transients instatic and astatic automatic control systems. The results of synthesis are confirmed by modeling with the help of a package Simulinkofthe system Matlab.

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Published

2018-01-10

Issue

Vol. 9 No. 2 (20) (2007): Вестник УГАТУ

Section

INFORMATICS, COMPUTER ENGINEERING AND MANAGEMENT