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Modern Missile Guidance, Second Edition

✍ Scribed by Rafael Yanushevsky


Publisher
CRC Press
Year
2018
Tongue
English
Leaves
343
Edition
2
Category
Library

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✦ Synopsis


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.

✦ Table of Contents


Cover......Page 1
Half Title......Page 2
Title Page......Page 4
Copyright Page......Page 5
Dedication......Page 6
Contents......Page 8
Preface......Page 12
Author......Page 16
1.1 Introduction......Page 18
1.2 Guidance Process......Page 20
1.3 Missile Guidance......Page 21
1.4 Representation of Motion......Page 22
1.5 Line-of-Sight......Page 24
References......Page 26
2.1 Introduction......Page 28
2.2 Proportional Navigation: Planar Engagement......Page 29
2.3 Proportional Navigation: Three-Dimensional Engagement......Page 31
2.4 Augmented Proportional Navigation......Page 32
2.5 Proportional Navigation as a Control Problem......Page 33
2.6 Augmented Proportional Navigation as a Control Problem......Page 36
2.7 When Is the PN Law Optimal?......Page 37
References......Page 38
3.1 Introduction......Page 40
3.2 Inertialess PN Guidance System......Page 41
3.3 Method of Adjoints......Page 42
References......Page 47
4.1 Introduction......Page 48
4.2 Adjoint Method: Generalized Model......Page 49
4.3 Frequency Domain Analysis......Page 53
4.5 Weave Maneuver Analysis......Page 60
4.6 Example......Page 62
4.7 Frequency Analysis and Miss Step Response......Page 63
4.8 Bounded Input–Bounded Output Stability......Page 67
4.9 Frequency Response of the Generalized Missile Guidance Model......Page 69
References......Page 71
5.1 Introduction......Page 74
5.2 Guidance Correction Controls......Page 75
5.3 Lyapunov Approach to Control Law Design......Page 76
5.4.1 Optimal Guidance for Nonmaneuvering Targets......Page 79
5.4.2 Optimal Augmented Guidance Laws......Page 82
5.5 Modified Linear Planar Model of Engagement......Page 83
5.6 General Planar Case......Page 84
5.7 Three-Dimensional Engagement Model......Page 87
5.8 Generalized Guidance Laws......Page 89
5.9 Examples......Page 93
References......Page 98
6.1 Introduction......Page 100
6.2 Neoclassical Missile Guidance......Page 101
6.3 Pseudo-Classical Missile Guidance......Page 105
6.4.1 Planar Model of Engagement......Page 108
6.4.2 Multidimensional Model of Engagement......Page 113
References......Page 115
7.1 Introduction......Page 116
7.2 Brief Discussion of Stochastic Processes......Page 117
7.3 Random Target Maneuvers......Page 121
7.4 Analysis of Influence of Noises on Miss Distance......Page 123
7.5 Effect of Random Target Maneuvers on Miss Distance......Page 127
7.6 Computational Aspects......Page 129
7.7 Examples......Page 131
7.8 Filtering......Page 142
References......Page 143
8.1 Introduction......Page 144
8.2 Basic Guidance Laws and Vision-Based Navigation......Page 146
8.3.1 Waypoint Guidance Problem......Page 153
8.3.2 Rendezvous Problem......Page 154
8.3.3 Conditional Rendezvous Problem......Page 157
8.4 Guidance of a Swarm of UAVs......Page 158
8.5 Obstacle Avoidance Algorithms......Page 161
References......Page 163
9.1 Introduction......Page 166
9.2 Forces Acting on Missile and Fixed-Wing UAV......Page 168
9.3 Missile and Fixed-Wing UAV Dynamics......Page 170
9.4 Reference Systems and Transformations......Page 174
9.5.1 Pitch Autopilot Design Model......Page 176
9.5.3 Roll Autopilot Design Model......Page 178
9.5.4 Actuators......Page 181
9.6 Missile Seekers......Page 182
9.7 Filtering and Estimation......Page 185
9.8 Kappa Guidance......Page 191
9.9 Lambert Guidance......Page 193
9.10 Simulation Models......Page 194
9.10.1 6-DOF Simulation Model......Page 196
9.10.2 3-DOF Simulation Models......Page 202
References......Page 207
10.1 Introduction......Page 208
10.2 Integrated Missile Guidance and Control Model......Page 210
10.3.1 Minimization of Standard Functionals......Page 219
10.3.2 Minimization of Special Functionals......Page 221
10.4 Integration and Decomposition......Page 225
References......Page 230
11.1 Introduction......Page 232
11.2 Kill Vehicles for Boost-Phase Defense......Page 234
11.3 Development of the Missile Model and Selection of Guidance Law Parameters......Page 237
11.4.1 Planar Model......Page 242
11.4.2 3-DOF Model: Nominal Trajectory......Page 247
11.4.3 3-DOF Model: Step and Weaving Target Maneuvers......Page 253
11.5.1 Interceptor’s Model......Page 256
11.5.2 Simulation Results: Non-Maneuvering Target......Page 259
11.5.3 Simulation Results: Influence of Shaping Term......Page 263
11.6.1 Axial Control of Kill Vehicle......Page 266
11.6.2 Axial Control of Interceptor......Page 270
11.7 Comparative Analysis with Lambert Guidance......Page 275
References......Page 278
12.1 Introduction......Page 280
12.2 Software for Frequency Domain Approach......Page 282
12.3 Software for Time Domain Methods......Page 293
References......Page 312
A.1 Lyapunov Method......Page 314
A.2 Bellman–Lyapunov Approach......Page 315
References......Page 318
B.2 Proof of Theorem......Page 320
Reference......Page 322
C.1 Aerodynamic Regression Models......Page 324
References......Page 325
D.1 Runge–Kutta Method......Page 326
Glossary......Page 330
Index......Page 334


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