The invention provides a novel control method for a high aspect-ratio flying wing solar-powered airplane. Through a steering engine, the tension line direction of a vector motor is controlled, the rotating speed of the motor is controlled and the deflection of a control surface is adjusted, so that the flying state of the airplane is controlled; and complicated control system and sensing system are simplified, so as to achieve the function of controlling the airplane. According to the control method, stable control on the high aspect-ratio flying wing solar-powered airplane can be finished; the control system can be simplified; the structure weight can be reduced; the working load of the airplane is improved; and the control reliability of the airplane is increased.
Novel control method for high aspect-ratio flying wing solar-powered airplane
2015-04-29
Patent
Elektronische Ressource
Englisch
Oblique-Flying-Wing Supersonic Transport Airplane
NTRS | 1992
|ADRC Flight Control System Design for Flying Wing UAV with High Aspect Ratio
Springer Verlag | 2024
|The light airplane and low-powered flying
Engineering Index Backfile | 1925
|CFD COMPUTATION OF THE GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING
British Library Conference Proceedings | 2012
|