Flying wing model lateral control device and control method

• Main Authors: LIU JIE, HU QIUQI, SUN JIAN, XU JINJING, NIU ZHONGGUO, CUI LIDONG
• Format: Patent
• Language: Chinese; English
• Published: 11.08.2017
• Subjects: CONTROLLING; PHYSICS; REGULATING; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES

The invention relates to the technical field of flying wing model control, and particularly relates to a flying wing model lateral control device and a control method. The device comprises a flying wing aircraft. A left wing plasma actuator and a right wing plasma actuator are respectively arranged at the outer edges of the front ends of the left and right rings of the flying wing aircraft. The plasma actuators are electrically connected with a controller through a short-pulse plasma high-voltage power supply and a relay. The controller is electrically connected with a gyroscope. Through controlling the plasma actuators of the two wings, the upward force of the aircraft can be increased during flight at a high angle of incidence and the aircraft can be prevented from losing speed. The flight attitude is adjusted in time and automatically during flight at a high angle of incidence. Thus, the phenomenon that an accident may be caused as the aircraft control surface is in a separation zone and cannot control the