Development of a flight control system using modern control techniques

Development of a flight control system using modern control techniques

The objective of this research project is to develop a practical bank-to-turn (BTT) missile autopilot system. BTT steering is preferred as it is capable of increasing the lift-to-drag ratio, thus increasing the magnitude of acceleration. A survey done reviewed that the majority of today's autop...

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Main Author: Ang, Kim Siah
Other Authors: Teoh, Earn Khwang
Format: Theses and Dissertations
Language:English
Published: 2009
Subjects:
DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
Online Access:http://hdl.handle.net/10356/19778
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Institution: Nanyang Technological University
Language: English
id sg-ntu-dr.10356-19778
record_format dspace
spelling sg-ntu-dr.10356-197782023-07-04T15:23:15Z Development of a flight control system using modern control techniques Ang, Kim Siah Teoh, Earn Khwang School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering The objective of this research project is to develop a practical bank-to-turn (BTT) missile autopilot system. BTT steering is preferred as it is capable of increasing the lift-to-drag ratio, thus increasing the magnitude of acceleration. A survey done reviewed that the majority of today's autopilots, both in missile systems and aircraft, are designed using classical control methods. With increasingly stringent mission requirements, there is a need to develop a high performance missile autopilot by using advance control techniques. Master of Engineering 2009-12-14T06:37:26Z 2009-12-14T06:37:26Z 1993 1993 Thesis http://hdl.handle.net/10356/19778 en Nanyang Technological University 165 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
spellingShingle DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
Ang, Kim Siah
Development of a flight control system using modern control techniques
description The objective of this research project is to develop a practical bank-to-turn (BTT) missile autopilot system. BTT steering is preferred as it is capable of increasing the lift-to-drag ratio, thus increasing the magnitude of acceleration. A survey done reviewed that the majority of today's autopilots, both in missile systems and aircraft, are designed using classical control methods. With increasingly stringent mission requirements, there is a need to develop a high performance missile autopilot by using advance control techniques.
author2 Teoh, Earn Khwang
author_facet Teoh, Earn Khwang
Ang, Kim Siah
format Theses and Dissertations
author Ang, Kim Siah
author_sort Ang, Kim Siah
title Development of a flight control system using modern control techniques
title_short Development of a flight control system using modern control techniques
title_full Development of a flight control system using modern control techniques
title_fullStr Development of a flight control system using modern control techniques
title_full_unstemmed Development of a flight control system using modern control techniques
title_sort development of a flight control system using modern control techniques
publishDate 2009
url http://hdl.handle.net/10356/19778
_version_ 1772828005955010560

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