Advances in Missile Guidance, Control, and Estimation

Author:   S.N. Balakrishnan (Missouri University of Science and Technology, Rolla, USA) ,  A. Tsourdos (Cranfield University, Swindon, UK) ,  B.A. White (Cranfield University, Swindon, UK) ,  B.A. White (Cranfield University, Shrivenham Wilts, UK)
Publisher:   Taylor & Francis Ltd
ISBN:  

9781138072954


Pages:   720
Publication Date:   29 March 2017
Format:   Paperback
Availability:   In Print   Availability explained
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Advances in Missile Guidance, Control, and Estimation


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Overview

Stringent demands on modern guided weapon systems require new approaches to guidance, control, and estimation. There are requirements for pinpoint accuracy, low cost per round, easy upgrade paths, enhanced performance in counter-measure environments, and the ability to track low-observable targets. Advances in Missile Guidance, Control, and Estimation brings together in one volume the latest developments in the three major missile-control components—guidance, control, and estimation—as well as advice on implementation. It also shows how these elements contribute to the overall missile design process. Shares Insights from Well-Known Researchers and Engineers from Israel, Korea, France, Canada, the UK, and the US The book features contributions by renowned experts from government, the defense industry, and academia from the United States, Israel, Korea, Canada, France, and the United Kingdom. It starts from the ground up, developing equations of missile motion. It reviews the kinematics of the engagement and the dynamics of the target and missile before delving into autopilot design, guidance, estimation, and practical implementation issues. Covers Nonlinear Control Techniques as Well as Implementation Issues The book discusses the design of autopilots using new nonlinear theories and analyzes the performance over a flight envelope of Mach number and altitude. It also contains a chapter on the recent integrated-guidance-and-control approach, which exploits the synergy between the autopilot and guidance system design. The book then outlines techniques applied to the missile guidance problem, including classical guidance, sliding mode-based, and differential game-based techniques. A chapter on the use of differential games integrates the guidance law with the estimation of the target maneuver. A chapter on particle filter describes the latest development in filtering algorithms. The final chapters—written by engineers working in the defense industry in the US, Israel, and Canada—consider the design and implementation issues of a command-to-line-of-sight guidance system and autopilots. An Invaluable Resource on the State of the Art of Missile Guidance A guide to advanced topics in missile guidance, control, and estimation, this invaluable book combines state-of-the-art theoretical developments presented in a tutorial form and unique practical insights. It looks at how tracking, guidance, and autopilot algorithms integrate into a missile system and guides control system designers through the challenges of the design process.

Full Product Details

Author:   S.N. Balakrishnan (Missouri University of Science and Technology, Rolla, USA) ,  A. Tsourdos (Cranfield University, Swindon, UK) ,  B.A. White (Cranfield University, Swindon, UK) ,  B.A. White (Cranfield University, Shrivenham Wilts, UK)
Publisher:   Taylor & Francis Ltd
Imprint:   CRC Press
Weight:   1.330kg
ISBN:  

9781138072954


ISBN 10:   1138072958
Pages:   720
Publication Date:   29 March 2017
Audience:   Professional and scholarly ,  Professional & Vocational
Format:   Paperback
Publisher's Status:   Active
Availability:   In Print   Availability explained
This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us.

Table of Contents

Robust Autopilot Design for Quasilinear Parameter-Varying Missile Model. Polynomial Approach for Design and Robust Analysis of Lateral Missile Control. Control Design and Gain Scheduling Using Observer-Based Structures. Adaptive Neural Network–Based Autopilot Design. Integrated Guidance and Control for Missiles. Higher-Order Sliding Modes for Missile Guidance and Control. Neoclassical Missile Guidance. Differential Geometry Applied to Missile Guidance. Differential Game-Based Interceptor Missile Guidance. Practical Techniques for the Design of Multirate Digital Guidance Laws and Autopilots. Optimal Guidance Laws with Impact Angle Control. Integrated Design of Estimator and Guidance Law. Introduction to Particle Filters for Tracking and Guidance. Design of CLOS Guidance System. Practical Considerations in Robust Control of Missiles. Index.

Reviews

...Advances in Missile Guidance, Control and Estimation is an edited collection of chapters each written by experts in the field... The introduction develops the missile equations of motion and homing engagement dynamics before introducing autopilot and guidance algorithm development; it then poses some challenges and finishes by summarising the contents of the book. -The Aeronautical Journal, January 2013


...Advances in Missile Guidance, Control and Estimation is an edited collection of chapters each written by experts in the field... The introduction develops the missile equations of motion and homing engagement dynamics before introducing autopilot and guidance algorithm development; it then poses some challenges and finishes by summarising the contents of the book. -The Aeronautical Journal, January 2013


"""…Advances in Missile Guidance, Control and Estimation is an edited collection of chapters each written by experts in the field… The introduction develops the missile equations of motion and homing engagement dynamics before introducing autopilot and guidance algorithm development; it then poses some challenges and finishes by summarising the contents of the book."" —The Aeronautical Journal, January 2013"


Author Information

A. Tsourdos, S.N. Balakrishnan, B.A. White

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