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UUM 514E
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Course Information
Course Name
Turkish
Helikopter Stabilite ve Kontrolü
English
Helicopter Stability and Control
Course Code
UUM 514E
Credit
Lecture
(hour/week)
Recitation
(hour/week)
Laboratory
(hour/week)
Semester
1
3
3
-
-
Course Language
English
Course Coordinator
İsmail Bayezit
Course Objectives
Course Objectives are listed as follows:
1 Dynamics of Rotorcraft and Multicopter Systems
2 Multicopter Modeling and Control
3 Calculation of Stability Derivatives and Aerodynamic Flight Parameters
4 To perform trim analysis and different control methods
Course Description
Basic terminology, simplified performance analysis, general equations of motion, rotor dynamics, rotor wake and inflow dynamics, rotor forces and moments, simplified trim analysis, linearized equations of motion, stability and control derivatives, static stability and control characteristics, dynamic stability, handling qualities, flight control systems are considered for rotorcraft systems.
Course Outcomes
Course outcomes are as follows:
1 Recognize rotorcraft/multirotor equations of motion.
2 Stability and Control Characteristics
3 Able to do trim analysis
4 Can calculate stability and control derivatives
5 Dynamic Stability Conditions
6 Flight Control Systems.
Pre-requisite(s)
Students are required to have a working knowledge of
- Engineering Mathematics (Differential Calculus)
- Linear Algebra
- Dynamics
- Fundamental understanding of Physics and Electrical/Electronic systems
- Introduction to Control
Required Facilities
Matlab/Simulink knowledge or LMS AMESim/AMESet knowledge for multi-physical modeling of rotorcraft mechanism.
Other
Textbook
1- Raymond W. Prouty, Helicopter, Performance, Stability, and Control, PWS Publishing, Original Edition, ISBN 0-534-06360-8, 1986
2- J. Seddon, Simon Newman, Basic Helicopter Aerodynamics, 2nd Edition, 2002
3- Richard C. Dorf, Robert H. Bishop, Modern Control Systems, 12 Edition, 2010.
Other References
1- Leishman, G., 2006. Principles of Helicopter Aerodynamics, Cambridge Aerospace Series, ISBN 0-521-85860-7.
2- Stanley, J.D., 1984. Helicopter Design and Data Book, Aviation Publications.
3- Engineering Design Handbook, 1974. Helicopter Engineering, Part One - Preliminary Design, AMC Pamphlet 706-201, HQS, U.S. Army Materiel Command, Aug 1974.
4- Padfield, G.D., 1995. Helicopter Flight Dynamics: The theory and application of flying qualities and simulation modelling. AIAA Education series.
5- Higgins L.B. and Hanks, M.L. 1991. Rotary Wing Stability and Control, USNTPS-FTM-NO.107.
6- Johnson, W., 1994. Helicopter Theory, Dover Publications, ISBN-0-486-68230-7
7- Bramwell, A.R.S., 1976. Helicopter Dynamics, Edward Arnold Pub., London.
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