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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Bibliographic Details
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
Description
Summary: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.

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