5643 UAV SYSTEMS I
The course presents the fundamentals of modelling the dynamics of rotorcraft-based
Unmanned Aerial Vehicle systems taught in the Department of Aerospace Information Engineering
Konkuk University, Korea. Upon finishing the course, the students are expected
to have a good understanding of key dynamic characteristics of RUAVs. The course
emphasizes the importance of an accurate yet simple enough model to be practical for
control design and analysis
Course topics
- Introduction to Rotorcraft-based Unmanned Aerial Vehicles: mission, operation and design specification
- Dynamics of Rotorcraft-based Unmanned Aerial Vehicles
- Euler-Newton equations of motion
- Forces and moments of helicopter: main rotor, tail rotor, vertical tail fin, horizontal tail
- Trim conditions: Hover and Cruise
- Linearization of equation of motion and principle of small perturbation
- Methods for calculation of stability derivatives: stability derivatives during hover and cruise
- Stability analysis of small scale helicopter
- Classical control design: description of proportional derivative controller
- Introduction to Modern control: Optimal control vs Algebraic Approach
- Squared-Coefficient Diagram Method (s-CDM) for Hover Control
- Aggressive maneuvering, hybrid approach to modelling and control
- Course syllabus pdf
- Advances in Unmanned Aerial Vehicles Technologies, International Symposium on Intelligent Unmanned System, ISIUS2008, Nanjing, China, October 15-18, 2008 pdf
- Optimal Tracking Controller Design for a Small Scale Helicopter, Journal of Bionic Engineering 4 (2007) 271-280 pdf
- First Principle Approach to Modeling of Small Scale Helicopter. International Conference on Intelligent Unmanned System, ICIUS, Bali, October 24-25, 2007 pdf
- An Algebraic Approach for the MIMO Control of Small Scale heli. International Conference on Intelligent Unmanned System, ICIUS, Bali, October 24-25, 2007 pdf
- Budiyono, A., Design and Development of Autonomous Uninhabited Air Vehicles at ITB: Challenges and Progress Status. Paper presented at the Aerospace Indonesia Meeting, Bandung, Indonesia 27 July 2005 pdf
