MathCad software development for research of controlled longitudinal motion of an aircraft on landing
UDC 692.7.05.001 BBK 39.571.552
The article describes the main aircraft control techniques and presents a technology and an algorithm of exploring the controlled longitudinal dynamics on aircraft landing in the MathCad environment. The research is carried out under the action of different control laws of the automatic control system on approach by means of computational modeling of the aircraft controlled longitudinal dynamics.
Key words: landing system, automatic control system, director control system, MathCad, mathematical model, aircraft, the phase of landing, modeling.
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