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The possibilities of optimization of the control elements in the cabin of the L-39NG aircraft
Klečák, Filip ; Zikmund, Pavel (referee) ; Procházková, Hana (advisor)
An effective cockpit design is one of the main prerequites for creating a succesful aircraft. This statement is even more pronounced in the sphere of military aviation, where perfect synergy is usually required between the pilot and the aircraft. This thesis focuses on optimization of control elements in the cockpit of the Aero L-39NG aircraft, a new trainer airplane designed by the czech company Aero Vodochody AEROSPACE. This airplane belongs to the jet trainer airplane category, representing an important role in training military pilots progressing towards fighter airplanes. The chosen method of conduction is a research of similar trainer airplanes as well as modern fighter airplanes, examination and comparison of used control elements and equipment. The main objective is to create suggestions of possible cockpit opimizations according to the trends observed in the studied aircraft.

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