| Code |
15257
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| Year |
1
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| Semester |
S2
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| ECTS Credits |
6
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| Workload |
PL(20H)/TP(40H)
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| Scientific area |
Aeronautics and Astronautics
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|
Entry requirements |
-
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Learning outcomes |
• Knowing the principles of parametric identification of dynamical systems, with applications to aircraft flight dynamics;
• Knowing how to specify and to model controller requirements for SISO and MIMO systems;
• Knowing how to design, implement and computationally validate flight controllers.
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Syllabus |
Part I (Parametric Identification) – Principles of parametric identification. Identification of longitudinal flight dynamics. Identification of lateral-directional flight dynamics.
Part II (Flight Control) – Models and Analysis of dynamical systems. Controller design for SISO systems (PID and compensators). Controller design for MIMO systems (LQR and H-infinity).
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Main Bibliography |
1. E. Hendricks, O. Jannerup, and P.H. Sorensen, Linear Systems Control, Springer, 2008.
2. F. L. Lewis and V. L. Syrmos, Optimal Control, John Wiley & Sons, 1995.
3. D. McLean. Automatic Flight Control Systems. Prentice Hall, 1990.
4. A. V. Rao. A Survey of Numerical Methods for Optimal Control, Advances in the Astronautical Sciences Series, Vol. 135, Paper AAS 09-334, 2010.
5. L. Ljung. System Identification – Theory for the User, 2nd Edition, Prentice Hall, 1999.
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Teaching Methodologies and Assessment Criteria |
ASSESSMENT CRITERIA:
A. LEARNING PHASE
Tutorial Lectures (20%)
Two Tests: (2 x 20%)
Two Miniprojects: (2 x 20%).
B. CONDITION FOR ADMISSION TO THE EXAM: have an average mark of at least 6/20 during the learning phase.
C. EXAM: Written exam (100%).
D. Final Mark: the highest mark in the learning phase and in the exam, comparatively.
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Language |
Portuguese. Tutorial support is available in English.
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