Missile Guidance and Control Systems

Missile Guidance and Control Systems

Author: George M. Siouris

Publisher: Springer Science & Business Media

Published: 2006-05-07

Total Pages: 666

ISBN-13: 0387218165

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Airborne Vehicle Guidance and Control Systems is a broad and wide- angled engineering and technological area for research, and continues to be important not only in military defense systems but also in industrial process control and in commercial transportation networks such as various Global Positioning Systems (GPS). The book fills a long-standing gap in the literature. The author is retired from the Air Force Institute and received the Air Force's Outstanding Civilian Career Service Award.


Book Synopsis Missile Guidance and Control Systems by : George M. Siouris

Download or read book Missile Guidance and Control Systems written by George M. Siouris and published by Springer Science & Business Media. This book was released on 2006-05-07 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Airborne Vehicle Guidance and Control Systems is a broad and wide- angled engineering and technological area for research, and continues to be important not only in military defense systems but also in industrial process control and in commercial transportation networks such as various Global Positioning Systems (GPS). The book fills a long-standing gap in the literature. The author is retired from the Air Force Institute and received the Air Force's Outstanding Civilian Career Service Award.


Design of Guidance and Control Systems for Tactical Missiles

Design of Guidance and Control Systems for Tactical Missiles

Author: Qi Zaikang

Publisher: CRC Press

Published: 2019-09-09

Total Pages: 261

ISBN-13: 1000681211

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Design of Guidance and Control Systems for Tactical Missiles presents a modern, comprehensive study of the latest design methods for tactical missile guidance and control. It analyzes autopilot designs, seeker system designs, guidance laws and theories, and the internal and external disturbances affecting the performance factors of missile guidance control systems. The text combines detailed examination of key theories with practical coverage of methods for advanced missile guidance control systems. It is valuable content for professors and graduate-level students in missile guidance and control, as well as engineers and researchers who work in the area of tactical missile guidance and control.


Book Synopsis Design of Guidance and Control Systems for Tactical Missiles by : Qi Zaikang

Download or read book Design of Guidance and Control Systems for Tactical Missiles written by Qi Zaikang and published by CRC Press. This book was released on 2019-09-09 with total page 261 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design of Guidance and Control Systems for Tactical Missiles presents a modern, comprehensive study of the latest design methods for tactical missile guidance and control. It analyzes autopilot designs, seeker system designs, guidance laws and theories, and the internal and external disturbances affecting the performance factors of missile guidance control systems. The text combines detailed examination of key theories with practical coverage of methods for advanced missile guidance control systems. It is valuable content for professors and graduate-level students in missile guidance and control, as well as engineers and researchers who work in the area of tactical missile guidance and control.


Advances in Missile Guidance, Control, and Estimation

Advances in Missile Guidance, Control, and Estimation

Author: S.N. Balakrishnan

Publisher: CRC Press

Published: 2016-04-19

Total Pages: 720

ISBN-13: 1420083147

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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 Estimat


Book Synopsis Advances in Missile Guidance, Control, and Estimation by : S.N. Balakrishnan

Download or read book Advances in Missile Guidance, Control, and Estimation written by S.N. Balakrishnan and published by CRC Press. This book was released on 2016-04-19 with total page 720 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 Estimat


Missile Guidance and Pursuit

Missile Guidance and Pursuit

Author: N A Shneydor

Publisher: Elsevier

Published: 1998-01-01

Total Pages: 266

ISBN-13: 1782420592

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The continuing evolving capability of guided weapons demands ever more knowledge of their development. This modern and comprehensive book covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer. The text studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process. Mathematics at first-year university level is the only prerequisite. Acquaintance with feedback control theory would be helpful to the reader. Covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer Studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process


Book Synopsis Missile Guidance and Pursuit by : N A Shneydor

Download or read book Missile Guidance and Pursuit written by N A Shneydor and published by Elsevier. This book was released on 1998-01-01 with total page 266 pages. Available in PDF, EPUB and Kindle. Book excerpt: The continuing evolving capability of guided weapons demands ever more knowledge of their development. This modern and comprehensive book covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer. The text studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process. Mathematics at first-year university level is the only prerequisite. Acquaintance with feedback control theory would be helpful to the reader. Covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer Studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process


Modern Missile Guidance

Modern Missile Guidance

Author: Rafael Yanushevsky

Publisher: CRC Press

Published: 2018-09-17

Total Pages: 335

ISBN-13: 1351202936

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Missile Guidance, Second Edition provides a timely survey of missile control and guidance theory, based on extensive work the author has done using the Lyapunov approach. This new edition also presents the Lyapunov-Bellman approach for choosing optimal parameters of the guidance laws, and direct and inverse optimal problems are considered. This material is important for readers working in the areas of optimization and optimal theory. This edition also contains updated coverage of guidance and control system components, since the efficiency of guidance laws depends on their realization. The text concludes with information on the new generation of intercept systems now in development.


Book Synopsis Modern Missile Guidance by : Rafael Yanushevsky

Download or read book Modern Missile Guidance written by Rafael Yanushevsky and published by CRC Press. This book was released on 2018-09-17 with total page 335 pages. Available in PDF, EPUB and Kindle. Book excerpt: Missile Guidance, Second Edition provides a timely survey of missile control and guidance theory, based on extensive work the author has done using the Lyapunov approach. This new edition also presents the Lyapunov-Bellman approach for choosing optimal parameters of the guidance laws, and direct and inverse optimal problems are considered. This material is important for readers working in the areas of optimization and optimal theory. This edition also contains updated coverage of guidance and control system components, since the efficiency of guidance laws depends on their realization. The text concludes with information on the new generation of intercept systems now in development.


Tactical and Strategic Missile Guidance

Tactical and Strategic Missile Guidance

Author: Paul Zarchan

Publisher: AIAA (American Institute of Aeronautics & Astronautics)

Published: 1997

Total Pages: 650

ISBN-13:

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For both experts and novices, presents the principles of both tactical and strategic missile guidance in a common language, notation, and perspective, with numerous examples to illustrate the concepts. This revised edition (1st ed., 1990) adds three new chapters on the fundamentals of endoatmospheric ballistic targets; a new chapter showing how covariance analysis can be used to analyze missile guidance systems; two new appendices; and included Macintosh and IBM compatible formatted disks containing the FORTRAN code listings presented in the text. Annotation copyright by Book News, Inc., Portland, OR


Book Synopsis Tactical and Strategic Missile Guidance by : Paul Zarchan

Download or read book Tactical and Strategic Missile Guidance written by Paul Zarchan and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1997 with total page 650 pages. Available in PDF, EPUB and Kindle. Book excerpt: For both experts and novices, presents the principles of both tactical and strategic missile guidance in a common language, notation, and perspective, with numerous examples to illustrate the concepts. This revised edition (1st ed., 1990) adds three new chapters on the fundamentals of endoatmospheric ballistic targets; a new chapter showing how covariance analysis can be used to analyze missile guidance systems; two new appendices; and included Macintosh and IBM compatible formatted disks containing the FORTRAN code listings presented in the text. Annotation copyright by Book News, Inc., Portland, OR


Design of Guidance and Control Systems for Tactical Missiles

Design of Guidance and Control Systems for Tactical Missiles

Author: Qi Zaikang

Publisher: CRC Press

Published: 2019-09-09

Total Pages: 240

ISBN-13: 1000680673

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Design of Guidance and Control Systems for Tactical Missiles presents a modern, comprehensive study of the latest design methods for tactical missile guidance and control. It analyzes autopilot designs, seeker system designs, guidance laws and theories, and the internal and external disturbances affecting the performance factors of missile guidance control systems. The text combines detailed examination of key theories with practical coverage of methods for advanced missile guidance control systems. It is valuable content for professors and graduate-level students in missile guidance and control, as well as engineers and researchers who work in the area of tactical missile guidance and control.


Book Synopsis Design of Guidance and Control Systems for Tactical Missiles by : Qi Zaikang

Download or read book Design of Guidance and Control Systems for Tactical Missiles written by Qi Zaikang and published by CRC Press. This book was released on 2019-09-09 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design of Guidance and Control Systems for Tactical Missiles presents a modern, comprehensive study of the latest design methods for tactical missile guidance and control. It analyzes autopilot designs, seeker system designs, guidance laws and theories, and the internal and external disturbances affecting the performance factors of missile guidance control systems. The text combines detailed examination of key theories with practical coverage of methods for advanced missile guidance control systems. It is valuable content for professors and graduate-level students in missile guidance and control, as well as engineers and researchers who work in the area of tactical missile guidance and control.


Principles of Guided Missiles and Nuclear Weapons

Principles of Guided Missiles and Nuclear Weapons

Author: United States. Bureau of Naval Personnel

Publisher:

Published: 1966

Total Pages: 376

ISBN-13:

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Fundamentals of missile and nuclear weapons systems are presented in this book which is primarily prepared as the second text of a three-volume series for students of the Navy Reserve Officers' Training Corps and the Officer Candidate School. Following an introduction to guided missiles and nuclear physics, basic principles and theories are discussed with a background of the factors affecting missile flight, airframes, missile propulsion systems, control components and systems, missile guidance, guided missile ships and systems, nuclear weapons, and atomic warfare defense. In the area of missile guidance, further explanations are made of command guidance, beam-rider methods, homing systems, preset guidance, and navigational guidance systems. Effects of nuclear weapons are also described in categories of air, surface, subsurface, underwater, underground, and high-altitude bursts as well as various kinds of damages and injuries. Besides illustrations for explanation purposes, a table of atomic weights and a glossary of general terms are provided in the appendices.


Book Synopsis Principles of Guided Missiles and Nuclear Weapons by : United States. Bureau of Naval Personnel

Download or read book Principles of Guided Missiles and Nuclear Weapons written by United States. Bureau of Naval Personnel and published by . This book was released on 1966 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fundamentals of missile and nuclear weapons systems are presented in this book which is primarily prepared as the second text of a three-volume series for students of the Navy Reserve Officers' Training Corps and the Officer Candidate School. Following an introduction to guided missiles and nuclear physics, basic principles and theories are discussed with a background of the factors affecting missile flight, airframes, missile propulsion systems, control components and systems, missile guidance, guided missile ships and systems, nuclear weapons, and atomic warfare defense. In the area of missile guidance, further explanations are made of command guidance, beam-rider methods, homing systems, preset guidance, and navigational guidance systems. Effects of nuclear weapons are also described in categories of air, surface, subsurface, underwater, underground, and high-altitude bursts as well as various kinds of damages and injuries. Besides illustrations for explanation purposes, a table of atomic weights and a glossary of general terms are provided in the appendices.


Optimal Guidance and Its Applications in Missiles and UAVs

Optimal Guidance and Its Applications in Missiles and UAVs

Author: Shaoming He

Publisher: Springer Nature

Published: 2020-05-13

Total Pages: 214

ISBN-13: 3030473481

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This book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority.


Book Synopsis Optimal Guidance and Its Applications in Missiles and UAVs by : Shaoming He

Download or read book Optimal Guidance and Its Applications in Missiles and UAVs written by Shaoming He and published by Springer Nature. This book was released on 2020-05-13 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority.


Differential Game Theory with Applications to Missiles and Autonomous Systems Guidance

Differential Game Theory with Applications to Missiles and Autonomous Systems Guidance

Author: Farhan A. Faruqi

Publisher: John Wiley & Sons

Published: 2017-05-30

Total Pages: 228

ISBN-13: 1119168473

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Differential Game Theory with Applications to Missiles and Autonomous Systems explains the use of differential game theory in autonomous guidance and control systems. The book begins with an introduction to the basic principles before considering optimum control and game theory. Two-party and multi-party game theory and guidance are then covered and, finally, the theory is demonstrated through simulation examples and models and the simulation results are discussed. Recent developments in the area of guidance and autonomous systems are also presented. Key features: Presents new developments and how they relate to established control systems knowledge. Demonstrates the theory through simulation examples and models. Covers two-party and multi-party game theory and guidance. Accompanied by a website hosting MATLABĀ® code. The book is essential reading for researchers and practitioners in the aerospace and defence industries as well as graduate students in aerospace engineering.


Book Synopsis Differential Game Theory with Applications to Missiles and Autonomous Systems Guidance by : Farhan A. Faruqi

Download or read book Differential Game Theory with Applications to Missiles and Autonomous Systems Guidance written by Farhan A. Faruqi and published by John Wiley & Sons. This book was released on 2017-05-30 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt: Differential Game Theory with Applications to Missiles and Autonomous Systems explains the use of differential game theory in autonomous guidance and control systems. The book begins with an introduction to the basic principles before considering optimum control and game theory. Two-party and multi-party game theory and guidance are then covered and, finally, the theory is demonstrated through simulation examples and models and the simulation results are discussed. Recent developments in the area of guidance and autonomous systems are also presented. Key features: Presents new developments and how they relate to established control systems knowledge. Demonstrates the theory through simulation examples and models. Covers two-party and multi-party game theory and guidance. Accompanied by a website hosting MATLABĀ® code. The book is essential reading for researchers and practitioners in the aerospace and defence industries as well as graduate students in aerospace engineering.