Dynamics of an aircraft augmented by direct control of aerodynamic forces and moments

• Autorzy: Gouskov Y. , Palyonov Y.
• Konferencja: Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

In this paper the novel forms of aircraft motion are demonstrated, using the simultaneous control over the aerodynamic forces and moments. These forms are similar to the well known old forms, in which the phase coordinates are kept constant, using traditional central control stick and pedals. The maneuvering capabilities of these old forms of motion can be increased, if parallel to the abovementioned controls the additional command devices are used. Using these additional command devices, pilot can generate additional signals to improve the longitudinal and lateral control of motion. By such a control the maneuvers can be separated into pure translation and pure rotation. This paper discusses the control systems for these maneuvers. It is shown that by the coordinated deflection of all aerodynamic control surfaces the pure (force-less) torque and the pure (torque-less) force can be provided.

Słowa kluczowe

EN

aircrafts; aerodynamic forces; maneuver aircraft

PL

samoloty; siły aerodynamiczne; manewry samolotu

• Wydawca: Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology
• Czasopismo: Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics
• Rocznik: 2001
• Tom: nr 11
• Strony: 87--94
• Opis fizyczny: Bibliogr. 2 poz., rys., tab., wykr.

Twórcy

autor

Gouskov Y.

autor

Palyonov Y.

• Moscow State Aviation Institute - Technical University, Moscow, Russia