Open AccessTHE METHOD OF EVALUATION OF THE AIRCRAFT CONTROL SYSTEM
Author(s) -
Tomasz Rogalski,
B. Dołęga
Publication year - 2005
Publication title -
aviation
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.239
H-Index - 13
eISSN - 1822-4180
pISSN - 1648-7788
DOI - 10.3846/16487788.2005.9635901
Subject(s) - aviation , control system , control (management) , engineering , fly by wire , aeronautics , general aviation , flight control surfaces , computer science , automotive engineering , flight simulator , control engineering , simulation , aerospace engineering , aerodynamics , artificial intelligence , electrical engineering
The dynamical development of general aviation demands compilation of new aircraft control methods. Those methods allow people without special airborne qualifications to pilot these aircrafts. The main goals of such a control system are to reduce a pilot's load, to improve control precision, and to protect an aircraft against dangerous situations. There are many criterions applied to grading and describing an aircraft's flying characteristics and the handling qualities of general aviation airplanes equipped with classical mechanical control systems. But a modern, small, transport aircraft should be equipped with fly‐by‐wire control systems, and there are no clear, straight, rules rate and describe the handling qualities of small airplanes with fly‐by‐wire control systems. This paper presents a methodology created by the authors that classifies and compares the handling qualities of general aviation aircraft equipped with fly‐by‐wire control systems. It takes into consideration two parameters: pilot's effort during realization of ordered tasks and precision of his control.