WUSTL ESE 543 - Lecture 1 and 2 rev - Copy (131 pages)

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Lecture 1 and 2 rev - Copy



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Lecture 1 and 2 rev - Copy

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Pages:
131
School:
Washington University in St. Louis
Course:
Ese 543 - Control Systems Design by State Space Methods

Unformatted text preview:

ESE 543 Control System Design Using State Space Methods Class Outline 1 Review of classical methods 2 System modeling and analysis 3 System structural properties 4 State Feedback design 5 Output feedback design 5 Multivariable frequency domain analysis 6 Robustness Theory 7 Optimal Control Text Modern Control Theory W L Brogan Text Robust and Adaptive Control with Aerospace Applications Lavretsky and Wise K A Wise Alt Optimal Control Anderson and Moore 2 Topics 1 System modeling and analysis Linearization State space systems Linear vector spaces Basis vectors Gram Schimdt orthogonalization Transformations mappings canonical forms Range space null space rank Eigenvalues eigenvectors Singular values singular vectors State transition matrix Solution to state equations 3 K A Wise Topics cont 2 System structural properties Controllability Observability Duality Degree of controllability observability Poles zeros MIMO transmission zeros Stability Lyapunov stability Regions of asymptotic stability 4 K A Wise Topics cont 3 Feedback design Pole placement Stabilizability Observer feedback Detectability Pole placement using observer feedback Linear Quadratic Regulator Theory Robust Servomechanism Projective Control Theory 5 K A Wise Topics cont 4 Multivariable frequency domain analysis Multivariable Nyquist theorem Relationship between SISO and MIMO stability analysis Singular value frequency response analysis 5 Optimal Control Linear quadratic regulator 6 Robustness Theory Uncertainty modeling Small gain theorem 6 K A Wise Grading Policy Homework Computer Projects Midterm Exam Final Exam 30 20 25 25 Matlab Boeing Phone 314 232 4549 Cell 636 866 9162 Email kevin a wise boeing com wiseka wustl edu 7 K A Wise Lecture 1 Robust and Adaptive Control Challenges 4th Generation Escape System X 45A J UCAS Nonlinear Aero Large Uncertainties Nonlinear Control Effectors Limited Actuation Vulture II Solar Eagle X 36 Tailless Agility Research Aircraft Unstable In Multiple Axes Non minimum



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