Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/53736
Title: Gain design and verification of autopilot control loops for UVAs
Authors: Huang, Qian.
Keywords: DRNTU::Engineering::Aeronautical engineering
Issue Date: 2011
Abstract: In this master thesis, autopilot control system of a UAV has been developed. Before starting the control system design, general concepts of system response have been reviewed. This whole work is divided into two parts. In the first part, autopilot structures have been developed and its control gains have been computed through design routine based on linear state space models of UAV and requirements of system response. In the second part, verifications of designed autopilot system are implemented for both linear and non-linear simulation models. In the end, conclusions about the suitability and relevance of the designed control system and achieved performance have been discussed.
URI: http://hdl.handle.net/10356/53736
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Theses

Files in This Item:
File Description SizeFormat 
HuangQian11.pdf
  Restricted Access
5.31 MBAdobe PDFView/Open

Page view(s) 50

278
Updated on May 14, 2021

Download(s)

9
Updated on May 14, 2021

Google ScholarTM

Check

Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.