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Course Code
AAE6103
Course Name
Advanced Control Theory for Aircraft
Department
aae
School ID
polyu
Faculty
Faculty of Engineering
Credits
3 credits
Level
6 Pre-requisite/ Co-requisite/
课程简介
/ Indicative Syllabus Introduction of Flight control – nonlinearities, model uncertainties, wind disturbances. Linear control and analysis – state-space representation, state-space solutions, stability, controllability, observability, state feedback design, output feedback design. Nonlinear control and analysis – Lyapunov’s indirect and direct methods, invariant set theorem, Barbalat’s lemma. Backstepping – stabilization by backstepping. Input-output linearization – asymptotic tracking by input-output linearization, normal form and zero dynamics. Sliding control – sliding surface, disturbance rejection, robustness. Adaptive control – adaptive control for aircrafts, adaptive control for Euler- Lagrange systems. -- 1 of 3 --
目标
To provide students with theories of advanced flight control including linear and nonlinear analysis and control methodologies, backstepping, feedback linearization, sliding mode control, adaptive control.
先修要求
/ Co-requisite/ Exclusion N/A
Teaching Pattern
Methodology 1. The teaching and learning methods include lecture/tutorial sessions, homework assignments and mini project. 2. Scientific examples and problems are raised and discussed in class/tutorial sessions.