"Tactical and Strategic Missile Guidance" by Paul Zarchan
American Institute of Aeronautics and Astronautics. Progress in Astronautics and Aeronautics, Volume 239, Sixth Edition
AIAA | 2012 | ISBN: 1600868940 9781600868948 | 1095 pages | PDF | 28 MB
American Institute of Aeronautics and Astronautics. Progress in Astronautics and Aeronautics, Volume 239, Sixth Edition
AIAA | 2012 | ISBN: 1600868940 9781600868948 | 1095 pages | PDF | 28 MB
This book provides an in-depth look into tactical and strategic missile guidance, considering proven guidance methods from various points of view. The sixth edition includes six new chapters on topics related to improving missile guidance system performance and understanding key design concepts and tradeoffs. The book aims to lay the foundation for meeting today's new challenges facing guidance engineers. The book is an indispensable guide for both the expert and the novice.
In this edition, the new chapters feature: two new applications of the method of adjoints for mixed continuous-discrete systems, and a new guidance law that can be used to shape the interceptor trajectory against a stationary target. Also considered is both the problem of finding the minimum achievable miss distance of a radar homing missile and exploring practical techniques that can be used to achieve the minimum possible miss.
It includes: an introduction of the differential game guidance law with bounded controls and a demonstration of its performance improvements over conventional guidance laws under challenging conditions; techniques for graphically presenting strategic information on successful intercepts of an impulsive ballistic target being pursued by an impulsive interceptor; and an examination of two filtering options for the boost-phase intercept of a strategic target.
It offers a look into some of the guidance and control issues involved in enabling an air-launched interceptor carrying a highly maneuverable kinetic kill vehicle to perform an exoatmospheric intercept of a boosting threat target that is capable of traveling many thousands of kilometers.
Table of Contents
1. Numerical Techniques
2. Fundamentals of Tactical Missile Guidance
3. Method of Adjoints and the Homing Loop
4. Noise Analysis
5. Covariance Analysis and the Homing Loop
6. Proportional Navigation and Miss Distance
7. Digital Fading Memory Noise Filters in the Homing Loop
8. Advanced Guidance Laws
9. Kalman Filters and the Homing Loop
10. Tactical Zones
11. Strategic Considerations
12. Boosters
13. Lambert Guidance
14. Strategic Intercepts
15. Miscellaneous Topics
16. Ballistic Target Properties
17. Extended Kalman Filtering and Ballistic Coefficient Estimation
18. Ballistic Target Challenges
19. Multiple Targets
20. Weaving Targets
21. Representing Missile Airframe with Transfer Functions
22. Introduction to Flight Control Design
23. Three-Loop Autopilot
24. Trajectory Shaping Guidance
25. Filtering and Weaving Targets
26. Alternative Approaches to Guidance Law Development
27. Filter Bank Approach to Weaving Target Problem
28. Engagement Simulations in Three Dimensions
29. Advanced Adjoint Applications
30. Miscellaneous Tactical Missile Guidance Topics
31. Comparison of Differential Game Guidance with Optimal Guidance
32. Kinematics of Intercepting a Ballistic Target
33. Boost-Phase Filtering Options
34. Kill Vehicle Guidance and Control Sizing for Boost-Phase Intercept
Appendix: Additional Examples
Index
with TOC BookMarkLinks