Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/19778
Title: Development of a flight control system using modern control techniques
Authors: Ang, Kim Siah
Keywords: DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
Issue Date: 1993
Abstract: 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.
URI: http://hdl.handle.net/10356/19778
Rights: Nanyang Technological University
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:EEE Theses

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