Landing augmentation system for general aviation aircraft: analysis and simulation

• Autorzy: Gruszecki J. , Tomczyk A.
• Języki publikacji: EN

Abstrakty

EN

A concept of the perspective solution of the general aviation aircraft control system is presented. The main idea of the project is to use the specialized Fly-by-Wire (FBW) control system. Fly-by-Wire implies that the cockpit controls are not mechanically linked to aerodynamic surfaces but are used only as the commands generator for the automatic flight control system. The objective of the proposed control for the control system is to assist pilots with limited aviation training by: 1/automatic stabilization of the aircraft's attitude, altitude, airspeed, and heading and 2/ decoupling of the flight controls. The proposed idea is useful for general aviation aircraft with relative low approach speed and typical nose-wheel landing gear. In particular, the most difficult phase of flight, which is aircraft's landing, is taken into consideration. The presented solution is proposed as the Landing Augmentation System (LAS).

• Wydawca: Oficyna Wydawnicza Politechniki Wrocławskiej
• Czasopismo: Systems Science
• Rocznik: 1999
• Tom: Vol. 25, nr 4
• Strony: 63--70
• Opis fizyczny: Bibliogr. 11 poz., rys. 5,

Twórcy

autor

Gruszecki J.

autor

Tomczyk A.

• Rzeszów University of Technology Rzeszów, Poland