Title :
Design of robust flight controller with multi-objective constraints based on MATLAB
Author :
Zhang Qingjiang ; Wang Xinmin ; Li Yan
Author_Institution :
Coll. of Autom., Northwestern Polytech. Univ., Xi´an, China
Abstract :
Robust multi-objective state feedback controller for the longitudinal dynamics of an aircraft is designed in this paper. The controller satisfies the constrains of pole placement and mixed H2/H∞ conditions so that the aircraft can meet the transient response requirement as well as the robustness requirement. Simulation results show the aircraft has high resistance to the disturbance. Simultaneously, the time it takes to reaches the steady state is short enough.
Keywords :
aerospace control; mathematics computing; robust control; state feedback; Matlab; aircraft; longitudinal dynamics; robust flight controller design; state feedback controller; transient response; Aerospace control; Aircraft; Automation; MATLAB; Robustness; State feedback; Matlab; Multi-objective Constraint; Robust Flight Controller;
Conference_Titel :
Control Conference (CCC), 2010 29th Chinese
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-6263-6
