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DESIGNING A CONTROL SYSTEM FOR THE AUTONOMOUS SMALL SCALE HELICOPTER

Abstract

dc:description.abstract

Designing a control system for the autonomous small scale helicopter mainly consists of two parts. First, Identify the system model (Helicopter model) and the second part is designing the compensator. Modeling the helicopter can be achieved by either first principles modeling or black box modeling. Based on the Model obtained, different controlling techniques can be used to design a compensator to achieve stability. This thesis presents an easy and accurate method to design the control system for the autonomous small scale helicopter. The helicopter system is identified using experimental data (black box modeling) with the help of MATLAB system identification tool box. And then the compensator is designed by using the MATLAB control system tool box. Various controlling methods like PID (Proportional Integral and Derivative), LQG (Linear Quadratic Gaussian) and IMC (Internal Model Controller) are compared while tuning the system to achieve highstability. The stability of the system is measured by its step response. Finally the system is simulated and its functionality is verified in MATLAB simulink. Since this thesis is focusing on the stable hovering state of the helicopter, we developed a simulated control system for the swash plate of the helicopter. Swash plate is mainly responsible for the helicopter's dynamics in rotation about X body axis (Roll) and rotation about Y body axis (Pitch). So the control system is developed and simulated in order to control the roll and pitch angles of the helicopter. The results show that LQG method gives the better step response than IMC, PID methods.

Degree

thesis:*
Grantor dc:publisher
Temple University. Libraries
Year dc:date.issued
2010

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Sajja, Satish
Advisor dc:contributor.advisor
  • Helferty, John J.
Committee members dc:contributor.committeemember
  • Silage, Dennis
  • Bai, Li

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • IN COPYRIGHT- This Rights Statement can be used for an Item that is in copyright. Using this statement implies that the organization making this Item available has determined that the Item is in copyright and either is the rights-holder, has obtained permission from the rights-holder(s) to make their Work(s) available, or makes the Item available under an exception or limitation to copyright (including Fair Use) that entitles it to make the Item available.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Dc Identifier Other
864884890
OAI identifier oai:identifier
oai:scholarshare.temple.edu:20.500.12613/2293

Chain of custody

source
Harvested from
Temple University
Base URL
scholarshare.temple.edu/server/oai/request
Last updated
2026-07-27
Source record
OAI-PMH GetRecord
citation

Sajja, Satish. DESIGNING A CONTROL SYSTEM FOR THE AUTONOMOUS SMALL SCALE HELICOPTER. Temple University. Libraries, 2010. http://hdl.handle.net/20.500.12613/2293