Missile Guidance and Control Systems

摘要: Contents 1 Introduction References 2 The Generalized Missile Equations of Motion 2.1 Coordinate Systems 2.1.1 Transformation Properties Vectors 2.1.2 Linear Vector Functions 2.1.3 Tensors 2.1.4 Transformations 2.2 Rigid-Body 2.3 D'Alembert's Principle 2.4 Lagrange's for Rotating 3 Aerodynamic Forces and Coefficients 3.1 Relative to the Wind Axis System 3.2 Moment Representation 3.2.1 Airframe Characteristics Criteria 3.3 Design Mathematical Model 3.3.1 3.3.2 3.4 Guidance 3.4.1 Seeker Subsystem 3.4.2 Noise Inputs 3.4.3 Radar Target Tracking Signal 3.4.4 Infrared 3.5 Autopilots 3.5.1 Control Surfaces Actuators 3.6 English Bias 4 Tactical Laws 4.1 4.2 Intercept Techniques 4.2.1 Homing 4.2.2 Command Other Types 4.3 4.4 Derivation Fundamental 4.5 Proportional Navigation 4.6 Augmented 4.7 Three-Dimensional 4.8 Application Optimal Feedback with Quadratic Performance in 4.8.1 4.8.2 Filtering 4.8.3 4.8.4 4.9 End Game 5 Weapon Delivery 5.1 5.2 Definitions Acronyms Used 5.2.1 5.2.2 5.3 Requirements 5.3.1 Tactics Maneuvers 5.3.2 Aircraft Sensors 5.4 Navigation/Weapon 5.4.1 Fire Computer 5.5 Factors In.uencing Accuracy 5.5.1 Error Sensitivities 5.5.2 Modes 5.6 Unguided Weapons 5.6.1 5.6.2 Free-Fall 5.6.3 Release Point Computation Bombs 5.7 Bombing Problem 5.7.1 Conversion Ground Plane Miss Distance into Aiming 5.7.2 Multiple Impacts 5.7.3 Relationship Among REP, DEP, CEP 5.8 5.9 Covariance Analysis 5.10 Three-Degree-of-Freedom Trajectory 5.10.1 5.11 Guided 5.12 Integrated Flight 5.12.1 Situational Awareness/Situation Assessment (SA/SA) 5.12.2 Targeting 5.13 Air-to-Ground Attack Component 5.14 Bomb Steering 5.15 Earth Curvature 5.16 Launch Envelope 5.17 Considerations Pertaining Computations 6 Strategic Missiles 6.1 6.2 Two-Body 6.3 Lambert's Theorem 6.4 First-Order a Ballistic 6.4.1 Newtonian Inverse-Square Field Solution 6.4.2 Spherical Hit Equation 6.4.3 Coef.cients 6.4.4 Effect Rotation 6.5 Correlated Velocity Velocity-to-Be-Gained Concepts 6.5.1 6.5.2 6.5.3 6.5.4 During Atmospheric Phase 6.5.5 6.6 Force 6.6.1 6.6.2 Dynamics 6.7 Reentry 6.8 6.9 6.9.1 6.9.2 7 Cruise 7.1 7.2 Description<7.2.1 Functional Operation 7.2.2 Description 7.3 7.3.1 7.4 Terrain Contour Matching (TERCOM) 7.4.1 7.4.2 De.nitions 7.4.3 Terrain-Contour Concept 7.4.4 Data Correlation 7.4.5 Roughness 7.4.6 TERCOM Sources 7.4.7 Position Updating 7.5 NAVSTAR/GPS 7.5.1 GPS/INS Integration A Constants B Glossary Terms C List D Standard E Classi.cation F Past Present Tactical/Strategic F.1 Historical Background F.2 Unpowered Precision-Guided Munitions (PGM) G Conics G.1 Preliminaries G.2 General Conic Trajectories H Frequency Bands I Selected Index