Now showing items 1-6 of 6

    • Adaptive Neuro-Observer for Elastic Drive Systems 

      Jafari, Amir Hossein (2011-12)
      This work presents the design, implementation, testing, and validation of a Neural Network based observer for a real hardware elastic drive system. Diagonal recurrent neural network architecture and two types of controllers ...
    • CFD Based Airfoil Shape Optimization for Aerodynamic Drag Reduction 

      Khot, Mohammed Taha Shafiq (2012-05)
      Commercial airplanes generally follow specific flight profiles consisting of take-off, climb, cruise, descend and landing. These flight profiles essentially change the freestream conditions in which the aircrafts operate. ...
    • Design and Implementation of an Advanced Control and Guidance Algorithm of a Single Rotor Helicopter 

      Al-Omari, Muhannad A. R. I. (2013-06)
      In this thesis, a complete autopilot solution for the Joker 3 miniature helicopter was designed and implemented. A dynamic model, which sufficiently describes the Joker 3 helicopter in a wide range of flight conditions was ...
    • Design of Robust Controllers for a Rotary Wing Helicopter 

      Ahmed, Rabiya (2013-06)
      Due to inherent instability, parametric variations, changing properties during flight, and uncertainties in predicting aerodynamic coefficients, helicopter flight control requires strategies with enough robustness to cope ...
    • Modeling and Fuzzy Control of Modern Refrigeration System 

      Afzali, Sayyed Hesam Pour (2014-06)
      Current typical refrigeration systems work with on-off controllers in each of their components and their expansion valves are regulated mechanically which is quite inefficient. This issue resides in the core design of the ...
    • Non-Linear Modeling and Control of Unmanned Air Vehicle 

      Ramezani, Roozbeh Falah (2012-05)
      The aim of this thesis is to design and simulate a Dynamic Inversion based autopilot for a fixed wing aircraft. The autopilot provides the aircraft motion stability by commanding the different aircraft control surfaces and ...