Last edited by Vojind
Sunday, July 26, 2020 | History

2 edition of Guidance and control of tactical missiles. found in the catalog.

Guidance and control of tactical missiles.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Guidance and Control Panel.

Guidance and control of tactical missiles.

by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Guidance and Control Panel.

  • 369 Want to read
  • 15 Currently reading

Published by North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development in [Neuilly-sur-Seine, France] .
Written in English

    Subjects:
  • Guided missiles -- Control systems.,
  • Guided missiles -- Guidance systems.

  • Edition Notes

    Includes bibliographical references.

    SeriesAGARD lecture series -- no. 52
    The Physical Object
    Paginationv, 121 p. in various pagings :
    Number of Pages121
    ID Numbers
    Open LibraryOL20204134M

    The only book devoted exclusively to the Matador and Mace Tactical Missiles. The book reveals the story from the initial idea that became the first U.S. pilotless bomber, through the politically troubled development of the ever evolving deployment methods of the Matador and Mace Tactical Missiles. Missile Guidance and Control Systems George M. Siouris 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.

    A brief treatment of military missiles follows. For full treatment, see rocket and missile system. Propulsion, control, and guidance. Although missiles can be propelled by either liquid-fueled or solid-fueled rocket engines, solid fuel is preferred for military uses because it is less likely to explode and can be kept ready-loaded for quick launch. Such engines commonly propel tactical guided. Design of Guidance and Control Systems for Tactical Missiles ().pdf writen by Qi Zaikang, Lin Defu: Design of Guidance and Control Systems for Tactical Missiles presents a modern, comprehensive study of the latest design methods for tactical .

      "This volume considers the modern tactical missile, which has become a highly integrated package made up of many electronic, mechanical, electromechanical and pyrotechnic sub-systems. In addition to hardware, it also covers the guidance algorithm and workings of the missile autopilot. Guidance and Control Most homing missiles use a form of proportional navigation once the seeker has acquired the target. This simple but effective guidance law has been in use for more than four decades on most of the worlds operational homing mis-siles. With proportional navigation, acceleration commands are issued which.


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Guidance and control of tactical missiles by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Guidance and Control Panel. Download PDF EPUB FB2

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 cturer: CRC Press.

Get this from a library. Guidance and control of tactical missiles. [North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Guidance and Control Panel.]. This book offers a comprehensive and up-to-date account of the technology behind tactical and strategic missiles and the guidance, control, and instrumentation required to reach a given "target."Cited by: Description: 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. Summary 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. 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 : Qi Zaikang, Lin Defu.

Book Description. 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.

This book offers a comprehensive and up-to-date account of the technology behind tactical and strategic missiles and the guidance, control, and instrumentation required to reach a given "target.". Now, let’s take a look at the main systems that are currently being used to implement various guidance control rules in missiles.

Line Of Sight system Commonly referred to as the LOS system, this type of control system consists of three components: a reference point (usually a radar station), a missile, and a target. Missile guidance and control systems The intent of this book is to present the fundamental concepts of guided missiles, both tactical, and strategic and the guidance, control, and instrumenta- tion needed to acquire a target.

In essence, this book is. Guidance radar is a necessary part in a command guidance system. It is often adopted in short to medium range ground-to-air missile guidance to accurately track the target and determine the line-of-sight direction of the target.

The source of the noise in a radar receiver is mainly thermal noise. 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.

This book offers a comprehensive and up-to-date account of the technology behind tactical and strategic missiles and the guidance, control, and instrumentation required to reach a given "target."/5(2). The goal of guidance is to compute the command required in order to reach a desired target.

In aerospace systems, guidance is used in conjugation with navigation and control systems to provide commands such that the target is reached. Schematically the implementation of a guidance, navigation, and control (GN&C) system is shown in Figure 1 Cited by: 3. Design of Guidanceand 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.

Though originally inspired by military applications, the advent of missile guidance and control systems has led to applications in a variety of fields -- in robotics, industrial process control, and in commercial transportation networks such as Global Positioning System technology.

This book offers a comprehensive and up-to-date account of the technology behind tactical and strategic missiles 5/5(1). Flight control topics include types of flight control (tail, canard, wing, thrust vector, reaction jet) and flight control maneuver laws (skid‐to‐turn, bank‐to‐turn, rolling airframe).

Finally, a discussion is provided of the role of missile system simulation in the technology development and Author: Eugene L.

Fleeman. This book offers a comprehensive and up-to-date account of the technology behind tactical and strategic missiles and the guidance, control, and instrumentation required to reach a given "target."4/5(1).

This book offers a comprehensive and up-to-date account of the technology behind tactical and strategic missiles and the guidance, control, and instrumentation required to reach a.

The material in this book has been assembled to support a Lecture Series presented by the authors at Bolkesjo (Norway), Athens (Greece) and Rome (Italy).

The. The book provides strategies for improved interceptor performance and presents valuable problem-solving methods. Topics include numerical techniques, fundamentals of tactical missile guidance, tactical zones, and flight control design. The revised sixth edition includes two new applications of the method of adjoints for mixed continuous.

Guidance and control of tactical missiles. Item Preview remove-circle some content may be lost due to the binding of the book. Addeddate Call number ocn Camera Canon 5D line Engineering Science r Naval Postgraduate SchoolPages: Proportional navigation guidance is a popular technique used in a majority of tactical radar and infrared (IR) guided missiles because of its simplicity, effectiveness and ease of : Rafael Yanushevsky.