Rafael Yanushevsky's Modern Missile Guidance PDF

By Rafael Yanushevsky

ISBN-10: 1420062263

ISBN-13: 9781420062267

ISBN-10: 142006228X

ISBN-13: 9781420062281

Written by way of knowledgeable with greater than 30 years of expertise, glossy Missile advice includes new analytical effects, received via the writer, that may be used for research and layout of missile tips and keep watch over structures. This ebook covers not only new equipment neither is it basically a compilation of older tools, even though it comprises either. The publication discusses, in a logical development, with its transparent elucidation of the suggestions legislation, the complete box from missile dynamics to modeling and trying out missile information and regulate platforms. not like latest books that debate extremely simple and infrequently unrealistic counsel procedure types, this publication provides missile advice types that describe extra exactly the dynamics of the missile flight keep an eye on approach, making analytical effects greater in perform. The research of missile counsel procedure types within the time-domain and within the frequency-domain permits the iteration of other information legislation that complement one another. Taking smooth, rigorous process that ends up in superior functionality in missile counsel purposes, the ebook examines new suggestions legislation, and corresponding algorithms for producing and checking out those legislation, and comprises powerful new software program courses built by means of the writer. the writer offers an leading edge presentation of the theoretical elements of recent missile assistance that really probably can't be present in the other ebook. It delineates new principles that, as soon as crystallized, will considerably enhance missile platforms functionality.

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Extra info for Modern Missile Guidance

Example text

Linear feedback solution for minimal effort intercept rendezvous, and soft landing, AIAA Journal, 3, 8, 1542–1548, 1965. 2. , On asymptotic stability and instability of motion with respect to a part of the variables, Journal of Applied Mathematics and Mechanics, 35, 1, 19–30, 1971. 3. , Theory of Optimal Linear Multivariable Control Systems, Nauka, Moscow, 1973. 4. Yanushevsky, R. , New approach to guidance law design, Journal of Guidance, Control, and Dynamics, 28, 1, 162–166, 2005. 5. Zadeh, L.

The frequency analysis enables us to evaluate the miss without simulation of the guidance system. Moreover, the miss for weave maneuvers, which are more realistic than step maneuvers, can be analyzed directly from the analytical expressions for the frequency response given above. They allow us to examine the influence of the guidance system parameters on the missile system performance. 8 Relationship between the maximum miss and the flight control system time constant. 1) is more precise than the binomial model considered in References [6,10,11].

Theory of Optimal Linear Multivariable Control Systems, Nauka, Moscow, 1973. 4. Yanushevsky, R. , New approach to guidance law design, Journal of Guidance, Control, and Dynamics, 28, 1, 162–166, 2005. 5. Zadeh, L. , Linear System Theory, McGraw Hill, New York, 1963. 6. , Washington, DC, 1997. 1 INTRODUCTION It is well known that investigation of processes and phenomena is linked, first of all, with the construction of mathematical models describing these processes and phenomena using mathematical language.

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Modern Missile Guidance by Rafael Yanushevsky

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