| Author | Thanis Nuchkrua |
| Call Number | AIT Thesis no. ISE-03-38 |
| Subject(s) | Flight control
|
| Note | A thesis submitted in partial fulfillment of the requirements for the
degree of Master of Engineering, School of Advanced Technologies |
| Publisher | Asian Institute of Technology |
| Series Statement | Thesis ; no. ISE-03-38 |
| Abstract | In this thesis we present the design, construction, implementation, simulation, and
control of a three degree of freedom hovering device capable of motion in the roll,
pitch, and yaw directions. This device provides the opp01tunity for exploration of a
variety of research related to dynamic systems. We first describe the design of the
system. Design procedures are outlined along with details of the construction of the
device. An identification of the system is presented for a Pitch Roll and yaw
subsystem, and the corresponding results of the model are employed in the
implementation of control algorithms. The electronic hardware detailed consists of a
PC data acquisition system and PWM signal amplifiers, computer software supplying
a real time software for control and data acquisition. Results of position control,
baseline control, and trajectory control are presented and analyzed. All of classical
control, PID results are compared with Optimal Control, LQR+Kalman filter solution. |
| Year | 2003 |
| Corresponding Series Added Entry | Asian Institute of Technology. Thesis ; no. ISE-03-38 |
| Type | Thesis |
| School | School of Advanced Technologies (SAT) |
| Department | Department of Civil and Infrastucture Engineering (DCIE) |
| Academic Program/FoS | Industrial Systems Engineering (ISE) |
| Chairperson(s) | Manukid Parnichkun; |
| Examination Committee(s) | Afzulpurkar, Nitin V.;
Bohez, Erik L.J. ; |
| Degree | Thesis (M.Eng.) - Asian Institute of Technology, 2003 |