| Introduction | p. 1 |
| References | p. 13 |
| The Generalized Missile Equations of Motion | p. 15 |
| Coordinate Systems | p. 15 |
| Transformation Properties of Vectors | p. 15 |
| Linear Vector Functions | p. 16 |
| Tensors | p. 17 |
| Coordinate Transformations | p. 18 |
| Rigid-Body Equations of Motion | p. 22 |
| D'Alembert's Principle | p. 45 |
| Lagrange's Equations for Rotating Coordinate Systems | p. 46 |
| References | p. 51 |
| Aerodynamic Forces and Coefficients | p. 53 |
| Aerodynamic Forces Relative to the Wind Axis System | p. 53 |
| Aerodynamic Moment Representation | p. 62 |
| Airframe Characteristics and Criteria | p. 77 |
| System Design and Missile Mathematical Model | p. 85 |
| System Design | p. 85 |
| The Missile Mathematical Model | p. 91 |
| The Missile Guidance System Model | p. 99 |
| The Missile Seeker Subsystem | p. 102 |
| Missile Noise Inputs | p. 113 |
| Radar Target Tracking Signal | p. 119 |
| Infrared Tracking Systems | p. 125 |
| Autopilots | p. 129 |
| Control Surfaces and Actuators | p. 144 |
| English Bias | p. 151 |
| References | p. 153 |
| Tactical Missile Guidance Laws | p. 155 |
| Introduction | p. 155 |
| Tactical Guidance Intercept Techniques | p. 158 |
| Homing Guidance | p. 158 |
| Command and Other Types of Guidance | p. 162 |
| Missile Equations of Motion | p. 174 |
| Derivation of the Fundamental Guidance Equations | p. 181 |
| Proportional Navigation | p. 194 |
| Augmented Proportional Navigation | p. 225 |
| Three-Dimensional Proportional Navigation | p. 228 |
| Application of Optimal Control of Linear Feedback Systems with Quadratic Performance Criteria in Missile Guidance | p. 235 |
| Introduction | p. 235 |
| Optimal Filtering | p. 237 |
| Optimal Control of Linear Feedback Systems with Quadratic Performance Criteria | p. 242 |
| Optimal Control for Intercept Guidance | p. 248 |
| End Game | p. 256 |
| References | p. 266 |
| Weapon Delivery Systems | p. 269 |
| Introduction | p. 269 |
| Definitions and Acronyms Used in Weapon Delivery | p. 270 |
| Definitions | p. 271 |
| Acronyms | p. 279 |
| Weapon Delivery Requirements | p. 284 |
| Tactics and Maneuvers | p. 286 |
| Aircraft Sensors | p. 289 |
| The Navigation/Weapon Delivery System | p. 290 |
| The Fire Control Computer | p. 292 |
| Factors Influencing Weapon Delivery Accuracy | p. 293 |
| Error Sensitivities | p. 294 |
| Aircraft Delivery Modes | p. 297 |
| Unguided Weapons | p. 299 |
| Types of Weapon Delivery | p. 300 |
| Unguided Free-Fall Weapon Delivery | p. 302 |
| Release Point Computation for Unguided Bombs | p. 304 |
| The Bombing Problem | p. 305 |
| Conversion of Ground Plane Miss Distance into Aiming Plane Miss Distance | p. 308 |
| Multiple Impacts | p. 312 |
| Relationship Among REP, DEP, and CEP | p. 314 |
| Equations of Motion | p. 314 |
| Covariance Analysis | p. 320 |
| Three-Degree-of-Freedom Trajectory Equations and Error Analysis | p. 323 |
| Error Analysis | p. 326 |
| Guided Weapons | p. 328 |
| Integrated Flight Control in Weapon Delivery | p. 332 |
| Situational Awareness/Situation Assessment (SA/SA) | p. 334 |
| Weapon Delivery Targeting Systems | p. 336 |
| Air-to-Ground Attack Component | p. 339 |
| Bomb Steering | p. 344 |
| Earth Curvature | p. 351 |
| Missile Launch Envelope | p. 353 |
| Mathematical Considerations Pertaining to the Accuracy of Weapon Delivery Computations | p. 360 |
| References | p. 364 |
| Strategic Missiles | p. 365 |
| Introduction | p. 365 |
| The Two-Body Problem | p. 366 |
| Lambert's Theorem | p. 382 |
| First-Order Motion of a Ballistic Missile | p. 389 |
| Application of the Newtonian Inverse-Square Field Solution to Ballistic Missile Flight | p. 389 |
| The Spherical Hit Equation | p. 392 |
| Ballistic Error Coefficients | p. 418 |
| Effect of the Rotation of the Earth | p. 440 |
| The Correlated Velocity and Velocity-to-Be-Gained Concepts | p. 443 |
| Correlated Velocity | p. 443 |
| Velocity-to-Be-Gained | p. 449 |
| The Missile Control System | p. 457 |
| Control During the Atmospheric Phase | p. 462 |
| Guidance Techniques | p. 466 |
| Derivation of the Force Equation for Ballistic Missiles | p. 472 |
| Equations of Motion | p. 477 |
| Missile Dynamics | p. 480 |
| Atmospheric Reentry | p. 482 |
| Missile Flight Model | p. 490 |
| Ballistic Missile Intercept | p. 504 |
| Introduction | p. 504 |
| Missile Tracking Equations of Motion | p. 515 |
| References | p. 519 |
| Cruise Missiles | p. 521 |
| Introduction | p. 521 |
| System Description | p. 527 |
| System Functional Operation and Requirements | p. 532 |
| Missile Navigation System Description | p. 534 |
| Cruise Missile Navigation System Error Analysis | p. 543 |
| Navigation Coordinate System | p. 548 |
| Terrain Contour Matching (TERCOM) | p. 551 |
| Introduction | p. 551 |
| Definitions | p. 555 |
| The Terrain-Contour Matching (TERCOM) Concept | p. 557 |
| Data Correlation Techniques | p. 563 |
| Terrain Roughness Characteristics | p. 568 |
| TERCOM System Error Sources | p. 570 |
| TERCOM Position Updating | p. 571 |
| The NAVSTAR/GPS Navigation System | p. 576 |
| GPS/INS Integration | p. 583 |
| References | p. 587 |
| Fundamental Constants | p. 589 |
| Glossary of Terms | p. 591 |
| List of Acronyms | p. 595 |
| The Standard Atmospheric Model | p. 605 |
| References | p. 609 |
| Missile Classification | p. 611 |
| Past and Present Tactical/Strategic Missile Systems | p. 625 |
| Historical Background | p. 625 |
| Unpowered Precision-Guided Munitions (PGM) | p. 644 |
| References | p. 650 |
| Properties of Conics | p. 651 |
| Preliminaries | p. 651 |
| General Conic Trajectories | p. 653 |
| References | p. 657 |
| Radar Frequency Bands | p. 659 |
| Selected Conversion Factors | p. 661 |
| Index | p. 663 |
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