The invention relates to aviation, and specifically to agile aircraft and to systems thereof for controlling said agile aircraft. The technical result to which the invention is directed consists in enhancing flight safety and the combat effectiveness of an aircraft by increasing diving time margins and, correspondingly, by extending the permissible centre-of-gravity position envelope, and by increasing the combat equipment resources of the aircraft, and also by realizing the optimum ratio of lifting force to drag. The agile aircraft comprises a fuselage (1), a sweptback wing (2), leading sweptback extensions (3), control members comprising a vertical fin (4) and a horizontal fin (5), and landing gear. The leading sweptback extensions (3) are arranged in the joining area between the nose part and middle part of the fuselage (1) and are equipped with controllable rotatable surfaces (6), wherein the axes of rotation of the front controllable surfaces (6) of the extensions (3) are arranged perpendicularly or at an angle to the longitudinal plane of the aircraft.
Agile aircraft
03.06.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Agile Fighter Aircraft Simulation
AIAA | 1989
|Intelligent Control of Agile Aircraft
British Library Conference Proceedings | 1999
|Human Consequences of Agile Aircraft
NTIS | 2000
Human consequences of agile aircraft
TIBKAT | 2000
Engine Characteristics for Agile Aircraft
British Library Conference Proceedings | 1994
|