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Design of robust flight controller with multi-objective constraints based on MATLAB

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3 Author(s)
Zhang Qingjiang ; Coll. of Autom., Northwestern Polytech. Univ., Xi'an, China ; Wang Xinmin ; Li Yan

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.

Published in:

Control Conference (CCC), 2010 29th Chinese

Date of Conference:

29-31 July 2010