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Tactical and Strategic Missile Guidance (Progress in Astronautics and Aeronautics), by Paul Zarchan
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This best-selling title 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. In addition, the original FORTRAN source code has now been converted into the widely used MATLAB programming language. The book aims to lay the foundation for meeting today's new challenges facing guidance engineers. In this latest 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. With numerous new examples and easy-to-understand graphs and explanations, "Tactical and Strategic Missile Guidance" is an indispensable guide for both the expert and the novice.
- Sales Rank: #817023 in Books
- Published on: 2013-09-18
- Original language: English
- Number of items: 1
- Dimensions: 9.30" h x 2.30" w x 6.40" l, 3.40 pounds
- Binding: Hardcover
- 1026 pages
Most helpful customer reviews
7 of 7 people found the following review helpful.
Comments From the author
By Paul Zarchan
The sixth edition has six new chapters on important topics related to improving missile guidance system performance and understanding key design concepts and tradeoffs. In addition, at the request of many readers, all of the FORTRAN source code that originally appeared in the first five editions of the text has been converted to MATLAB. However, as before, interested readers can obtain all of the texts MATLAB and equivalent FORTRAN versions of the MATLAB source code in electronic form from the AIAA website mentioned at the back of this text. The first new Chapter presents two new applications of the method of adjoints for mixed continuous-discrete systems. The first application involves multiple samplers with each of the samplers operating at a different sampling rate. The second application involves taking the adjoint of a three-state discrete Kalman filter in the homing loop. The second new Chapter introduces a new guidance law that can be used to shape the interceptor trajectory against a stationary target. The unique advantage of this new guidance approach over existing guidance laws is that time to go information is not required. The second part of the new Chapter considers 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. The third new Chapter introduces the differential game guidance law with bounded controls and demonstrates its performance improvements over conventional guidance laws under challenging conditions in which the missile to target acceleration advantage is very low. The fourth new Chapter introduces techniques for graphically presenting strategic information on successful intercepts of an impulsive ballistic target being pursued by an impulsive interceptor. The three graphical techniques discussed are the operational area method, the launch area denied method and the defended area method. Examples are presented illustrating the utility of each of three methods of presentation. The fifth new Chapter examines two filtering options for the boost phase intercept of a strategic target. The two filters compared are a template-based Kalman filter that has perfect a priori information and a linear three-state polynomial Kalman filter that does not require such information. The filters are compared under both ideal and realistic conditions. The results of this Chapter may surprise some readers. Finally, the sixth new Chapter addresses 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. This new Chapter takes the reader through the first iteration of the multi-iteration design process in order to show how much divert and acceleration may be required by the kinetic kill vehicle so that it can hit the target. Simplified examples are presented to indicate how conventional guidance and filtering techniques can be used as a starting point in the iterative design process for this important problem in missile defense.
1 of 1 people found the following review helpful.
Zarchan has written a primer that is about as perfect a survey of methods on the subject as one ...
By Raymond H. Smeeth
Zarchan has written a primer that is about as perfect a survey of methods on the subject as one could imagine. I've only bought three of his six editions, and I doubt, should he publish more, that I am done. Thanks, sir.
1 of 1 people found the following review helpful.
Five Stars
By Anthony Reid
What a great book for a semi-expert.
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