Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
A New Paradigm In Optimal Missile Guidance
Download A New Paradigm In Optimal Missile Guidance full books in PDF, epub, and Kindle. Read online A New Paradigm In Optimal Missile Guidance ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis A New Paradigm in Optimal Missile Guidance by : Robert W. Morgan
Download or read book A New Paradigm in Optimal Missile Guidance written by Robert W. Morgan and published by . This book was released on 2007 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt: This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of missile guidance usually lasts less than ten seconds and calls for very accurate maneuvering to ensure intercept. Technological advancements have produced increasingly sophisticated threats that greatly reduce the effectiveness of traditional approaches to missile guidance. Because of this, terminal missile guidance is, and will remain, an important and active area of research. The complexity of the problem and the desire for an optimal solution has resulted in researchers focusing on simplistic, usually linear, models. The fruit of these endeavors has resulted in some of the world's most advanced weapons systems. Even so, the resulting guidance schemes cannot possibly counter the evolving threats that will push the system outside the linear envelope for which they were designed. The research done in this dissertation greatly extends previous research in the area of optimal missile guidance. Herein it is shown that optimal missile guidance is fundamentally a pairing of an optimal guidance strategy and an optimal control strategy. The optimal guidance strategy is determined from a missile's information constraints, which are themselves largely determined from the missile's sensors. The optimal control strategy is determined by the missile's control constraints, and works to achieve a specified guidance strategy. This dichotomy of missile guidance is demonstrated by showing that missiles having different control constraints utilize the same guidance strategy so long as the information constraints are the same. This concept has hitherto been unrecognized because of the difficulty in developing an optimal control for the nonlinear set of equations that result from control constraints. Having overcome this difficulty by indirect means, evidence of the guidance strategy paradigm emerged. The guidance strategy paradigm is used to develop two advanced guidance laws. The new guidance laws are compared qualitatively and quantitatively with existing guidance laws.
Book Synopsis Modern Missile Guidance by : Rafael Yanushevsky
Download or read book Modern Missile Guidance written by Rafael Yanushevsky and published by CRC Press. This book was released on 2018-09-17 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Missile Guidance and Pursuit by : N A Shneydor
Download or read book Missile Guidance and Pursuit written by N A Shneydor and published by Elsevier. This book was released on 1998-01-01 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt: The continuing evolving capability of guided weapons demands ever more knowledge of their development. This modern and comprehensive book covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer. The text studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process. Mathematics at first-year university level is the only prerequisite. Acquaintance with feedback control theory would be helpful to the reader. Covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer Studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process
Book Synopsis Advances in Missile Guidance, Control, and Estimation by : S.N. Balakrishnan
Download or read book Advances in Missile Guidance, Control, and Estimation written by S.N. Balakrishnan and published by CRC Press. This book was released on 2016-04-19 with total page 720 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 Estimat
Author :Joseph Z. Ben-Asher Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :226 pages Book Rating :4.3/5 (91 download)
Book Synopsis Advances in Missile Guidance Theory by : Joseph Z. Ben-Asher
Download or read book Advances in Missile Guidance Theory written by Joseph Z. Ben-Asher and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1998 with total page 226 pages. Available in PDF, EPUB and Kindle. Book excerpt: Explores some new applications that are based on linear quadratic (LQ) theories to the optimal guidance problems. New guidance laws that are based on LQ one-sided optimization theory and on differential game theory are introduced, and old guidance laws are rederived and set in a more general framework. Written specifically for engineers, the problems are formulated and solved with state-space representations in an informal mathematical style. The disk includes the source code listings of the MATLAB and MAPLE subroutines for the analytical and numerical solutions to the optimization problems in the text. Annotation copyrighted by Book News, Inc., Portland, OR
Book Synopsis Optimal Control Applied to Missile Guidance by : Sandra Tierson Donohue
Download or read book Optimal Control Applied to Missile Guidance written by Sandra Tierson Donohue and published by . This book was released on 1979 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Missile Defense: Toward a New Paradigm by : Igor Ivanov
Download or read book Missile Defense: Toward a New Paradigm written by Igor Ivanov and published by . This book was released on 2022 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Paul Zarchan Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :650 pages Book Rating :4.3/5 (91 download)
Book Synopsis Tactical and Strategic Missile Guidance by : Paul Zarchan
Download or read book Tactical and Strategic Missile Guidance written by Paul Zarchan and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1997 with total page 650 pages. Available in PDF, EPUB and Kindle. Book excerpt: For both experts and novices, presents the principles of both tactical and strategic missile guidance in a common language, notation, and perspective, with numerous examples to illustrate the concepts. This revised edition (1st ed., 1990) adds three new chapters on the fundamentals of endoatmospheric ballistic targets; a new chapter showing how covariance analysis can be used to analyze missile guidance systems; two new appendices; and included Macintosh and IBM compatible formatted disks containing the FORTRAN code listings presented in the text. Annotation copyright by Book News, Inc., Portland, OR
Book Synopsis Optimal Missile Guidance by : Eddy Yong Chin Sim
Download or read book Optimal Missile Guidance written by Eddy Yong Chin Sim and published by . This book was released on 2000 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Optimal Control and Pathplanning in Missile Guidance Problems by : Johan Hamberg
Download or read book Optimal Control and Pathplanning in Missile Guidance Problems written by Johan Hamberg and published by . This book was released on 2004 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Optimal T-[Delta]v Guidance Law for Intercepting a Boosting Target by :
Download or read book An Optimal T-[Delta]v Guidance Law for Intercepting a Boosting Target written by and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Lawrence Livermore National Laboratory (LLNL) have developed a new missile guidance law for intercepting a missile during boost phase. Unlike other known missile guidance laws being used today, the new t-[Delta]v guidance law optimally trades an interceptor's onboard fuel capacity against time-to-go before impact. In particular, this guidance law allows a missile designer to program the interceptor to maximally impact a boosting missile before burnout or burn termination and thus negating its ability to achieve the maximum kinetic velocity. For an intercontinental range ballistic missile (ICBM), it can be shown that for every second of earlier intercept prior to burnout, the ICBM ground range is reduced by 350 km. Therefore, intercepting a mere 15 seconds earlier would result in amiss of 5,250 km from the intended target or approximately a distance across the continental US. This paper also shows how the t-[Delta]v guidance law can incorporate uncertainties in target burnout time, predicted intercept point (PIP) error, time-to-go error, and other track estimation errors. The authors believe that the t-[Delta]v guidance law is a step toward the development of a new and smart missile guidance law that would enhance the probability of achieving a boost phase intercept.
Book Synopsis A Method of Increasing the Kinematic Boundary of Air-to-Air Missiles Using an Optimal Control Approach by : Robert D. Broadston
Download or read book A Method of Increasing the Kinematic Boundary of Air-to-Air Missiles Using an Optimal Control Approach written by Robert D. Broadston and published by . This book was released on 2000-09-01 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt: Current missile guidance laws are generally based on one of several forms of proportional navigation (PN). While PN laws are robust, analytically tractable, and computationally simple, they are only optimal in a narrow operating regime. Consequently, they may not optimize engagement range, time to intercept, or endgame kinetic energy. The advent of miniaturized high speed computers has made it possible to compute optimal trajectories for missiles using command mid-course guidance as well as autonomous onboard guidance. This thesis employs a simplified six degree of freedom (6DOF) flight model and a full aerodynamic 6DOF flight model to analyze the performance of both PN and optimal guidance laws in a realistic simulation environment which accounts for the effects of drag and control system time constants on the missile's performance. Analysis of the missile's kinematic boundary is used as the basis of comparison. A missile's kinematic boundary can be described as the maximum theoretical range at which it can intercept a target assuming no noise in its sensors. This analysis is immediately recognizable to the warfighter as an engagement envelope. The guidance laws are tested against non-maneuvering and maneuvering aircraft targets and against a simulation of a cruise missile threat. An application of the 6DOF model for a theater ballistic missile interceptor is presented.
Book Synopsis Dissertation Abstracts International by :
Download or read book Dissertation Abstracts International written by and published by . This book was released on 2007 with total page 960 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Guidance, Control, and Tracking II by : Walter J. Fowski
Download or read book Space Guidance, Control, and Tracking II written by Walter J. Fowski and published by . This book was released on 1995 with total page 198 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Guidance, Control, and Tracking by :
Download or read book Space Guidance, Control, and Tracking written by and published by . This book was released on 1995 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1997 with total page 520 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 456 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
![Download An Optimal T-[Delta]v Guidance Law for Intercepting a Boosting Target PDF Online Free](https://books.google.com/books/content/images/frontcover/SzHRjwEACAAJ?fife=w200-h370)
