Title :
Lateral Directional Axis Control of Aircraft Based on TECS
Author :
Ke Ji ; Wang Wei ; Li Ai-jun ; Wang Chang-qing
Author_Institution :
Coll. of Autom., Northwestern Polytech. Univ., Xi´an, China
Abstract :
The principle of TECS (total energy control system) control-law is applied to the control of lateral directional axis of aircraft, utilizing the combination of bias control and total energy decoupling. Rolling mode and yawing mode are decoupled, and the control system with zero steady-state error is established. One type of aerotransport is simulated with aforementioned method. Simulation results show that the total energy control based on the longitudinal axis is capable for the lateral axis control. Accurate signal tracking of yaw angle and sideslip angle, as well as decoupling of rolling mode and yawing mode can be achieved.
Keywords :
aircraft control; power control; aerotransport; aircraft; bias control; control system; lateral directional axis control; rolling mode; total energy control system control law; total energy decoupling; yawing mode; zero steady-state error; Aerospace control; Aircraft; Automatic control; Automation; Control systems; Differential equations; Educational institutions; Elevators; Error correction; Steady-state;
Conference_Titel :
Image and Signal Processing, 2009. CISP '09. 2nd International Congress on
Conference_Location :
Tianjin
Print_ISBN :
978-1-4244-4129-7
Electronic_ISBN :
978-1-4244-4131-0
DOI :
10.1109/CISP.2009.5304509
