附註:Includes bibliographical references and index.
Cover -- Preface -- Table of Contents -- Chapter 1 Introduction -- References -- Chapter 2 The Generalized Missile Equations of Motion -- 2.1 Coordinate Systems -- 2.2 Rigid-Body Equations of Motion -- 2.3 D'Alembert's Principle -- 2.4 Lagrange's Equations for Rotating Coordinate Systems -- References -- Chapter 3 Aerodynamic Forces and Coefficients -- 3.1 Aerodynamic Forces Relative to the Wind Axis System -- 3.2 Aerodynamic Moment Representation -- 3.3 System Design and Missile Mathematical Model -- 3.4 The Missile Guidance System Model -- 3.5 Autopilots -- 3.6 English Bias -- References -- Chapter 4 Tactical Missile Guidance Laws -- 4.1 Introduction -- 4.2 Tactical Guidance Intercept Techniques -- 4.3 Missile Equations of Motion -- 4.4 Derivation of the Fundamental Guidance Equations -- 4.5 Proportional Navigation -- 4.6 Augmented Proportional Navigation -- 4.7 Three-Dimensional Proportional Navigation -- 4.8 Application of Optimal Control of Linear Feedback Systems with Quadratic Performance Criteria in Missile Guidance -- 4.9 End Game -- References -- 5 Weapon Delivery Systems -- 5.1 Introduction -- 5.2 Definitions and Acronyms Used in Weapon Delivery -- 5.3 Weapon Delivery Requirements -- 5.4 The Navigation/Weapon Delivery System -- 5.5 Factors Influencing Weapon Delivery Accuracy -- 5.6 Unguided Weapons -- 5.7 The Bombing Problem -- 5.8 Equations of Motion -- 5.9 Covariance Analysis -- 5.10 Three-Degree-of-Freedom Trajectory Equations and Error Analysis -- 5.11 Guided Weapons -- 5.12 Integrated Flight Control in Weapon Delivery -- 5.13 Air-to-Ground Attack Component -- 5.14 Bomb Steering -- 5.15 Earth Curvature -- 5.16 Missile Launch Envelope -- 5.17 Mathematical Considerations Pertaining to the Accuracy of Weapon Delivery Computations -- References -- Chapter 6 Strategic Missiles -- 6.1 Introduction -- 6.2 The Two-Body Problem -- 6.3 Lambert's Theorem -- 6.4 First-Order Motion of a Ballistic Missile -- 6.5 The Correlated Velocity and Velocity-to-Be-Gained
摘要: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 and the guidance, control, and instrumentation required to reach a given "target." Topics covered include: missile aerodynamic forces and moments, the missile mathematical model, weapon delivery, GPS (Global Positioning System) and TERCOM (terrain contour matching) guidance, cruise missile mechanization equations, and a detailed analysis of ballistic missile guidance laws. The presentation assumes familiarity with calculus, ordinary differential equations, and some knowledge of modern control theory. The text is replete wuith practical examples designed to illustrate important concepts. This book will be an essential resource for students of aeronautical/aerospace engineering, as well as practicing engineers involved in the design, development, and analysis of modern aerospace guidance and control systems
