The fifth edition of this best-selling title has three new chapters on important topics related to improving missile guidance performance and several important new concepts in the Appendix. The first new chapter presents several alternative ways of developing guidance laws numerically. These techniques can be used to derive more advanced guidance laws when the missile guidance system dynamics become very complex. An example is presented showing the advantages of a new advanced guidance law over more conventional guidance laws. Previous editions of the text have shown that intentional or unintentional spiraling maneuvers by a tactical ballistic missile can make it particularly difficult for a pursuing missile to hit.
Stringent demands on modern guided weapon systems require new approaches to guidance, control, and estimation. There are requirements for pinpoint accuracy, low cost per round, easy upgrade paths, enhanced performance in counter-measure environments, and the ability to track low-observable targets. Advances in Missile Guidance, Control, and Estimation brings together in one volume the latest developments in the three major missile-control components—guidance, control, and estimation—as well as advice on implementation. It also shows how these elements contribute to the overall missile design process. Shares Insights from Well-Known Researchers and Engineers from Israel, Korea, France, Canada, the UK, and the US The book features contributions by renowned experts from government, the defense industry, and academia from the United States, Israel, Korea, Canada, France, and the United Kingdom. It starts from the ground up, developing equations of missile motion. It reviews the kinematics of the engagement and the dynamics of the target and missile before delving into autopilot design, guidance, estimation, and practical implementation issues. Covers Nonlinear Control Techniques as Well as Implementation Issues The book discusses the design of autopilots using new nonlinear theories and analyzes the performance over a flight envelope of Mach number and altitude. It also contains a chapter on the recent integrated-guidance-and-control approach, which exploits the synergy between the autopilot and guidance system design. The book then outlines techniques applied to the missile guidance problem, including classical guidance, sliding mode-based, and differential game-based techniques. A chapter on the use of differential games integrates the guidance law with the estimation of the target maneuver. A chapter on particle filter describes the latest development in filtering algorithms. The final chapters—written by engineers working in the defense industry in the US, Israel, and Canada—consider the design and implementation issues of a command-to-line-of-sight guidance system and autopilots. An Invaluable Resource on the State of the Art of Missile Guidance A guide to advanced topics in missile guidance, control, and estimation, this invaluable book combines state-of-the-art theoretical developments presented in a tutorial form and unique practical insights. It looks at how tracking, guidance, and autopilot algorithms integrate into a missile system and guides control system designers through the challenges of the design process.
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.
This book is about terminal guidance of intercepting missiles. It contains a variety of newly developed guidance methods based on linear quadratic optimization problems. This application-oriented book employs widely used and thoroughly developed theories such as LQ and H-infinity to missile guidance. Numerous examples help the reader to gain greater understanding of the relative merits and shortcomings of the various methods. Both the analytical derivations and the numerical computations of the examples are carried out by MAPLE and MATLAB subroutines. The codes are provided with the book.
The biggest single increase in the U.S. defense budget request for modernization spending over the next six years is for ballistic missile defense, including theater and national systems. Engineers, managers, and policy makers will need to stay abreast of the ever-changing state of the art in theater ballistic missile defense. Very few books in the market cover the special technical and design issues involved in the development of a ballistic missile defense system. Drs. Naveh and Lorber pull together 40 years of experience in Israeli theater missile defense activities and provide in this single volume those special issues, state-of-the-design considerations, technologies, and procedures related to the theater ballistic missile defense arena.
Hermann Oberth gilt als einer der bedeutendsten Pioniere der Raketentechnik. Visionär waren nicht nur seine umfassende, akribische Untersuchung und Optimierung aller denkbaren Raketenparamter, sondern auch seine Vorschläge zur Raketeninstrumentierung für bemannte und wissenschaftliche Missionen sowie Ideen für Start- und Testanlagen. Die Neuauflage ermöglicht es, die Realisierung von Oberth's "Traum" nachzuvollziehen und mit der heutigen Raumfahrtrealität abzugleichen. Reprint der 5. Auflage von 1984
A practical guide to building Kalman filters, showing how the filtering equations can be applied to real-life problems. Numerous examples are presented in detail, and computer code written in FORTRAN, MATLAB and True BASIC accompanies all the examples.