INTERNATIONAL STANDARD BOOK NUMBER
(Number (ISBN
9781461489443
NATIONAL BIBLIOGRAPHY NUMBER
Country Code
IR
Number
EN-51681
LANGUAGE OF THE ITEM
.Language of Text, Soundtrack etc
انگلیسی
COUNTRY OF PUBLICATION OR PRODUCTlON
Country of publication
IR
TITLE AND STATEMENT OF RESPONSIBILITY
Title Proper
Optimal control with aerospace applications
General Material Designation
[Book]
First Statement of Responsibility
/ James M. Longuski, Jose J. Guzm?n, John E. Prussing
.PUBLICATION, DISTRIBUTION, ETC
Place of Publication, Distribution, etc.
New York, NY
Name of Publisher, Distributor, etc.
: Springer,
Date of Publication, Distribution, etc.
, 2014.
SERIES
Series Title
(Space technology library)
NOTES PERTAINING TO PUBLICATION, DISTRIBUTION, ETC.
Text of Note
Electronic
INTERNAL BIBLIOGRAPHIES/INDEXES NOTE
Text of Note
Includes bibliographical references and index..
CONTENTS NOTE
Text of Note
Summary: Want to know not just what makes rockets go up but how to do it optimally? Optimal control theory has become such an important field in aerospace engineering that no graduate student or practicing engineer can afford to be without a working knowledge of it. This is the first book that begins from scratch to teach the reader the basic principles of the calculus of variations, develop the necessary conditions step-by-step, and introduce the elementary computational techniques of optimal control. This book, with problems and an online solution manual, provides the graduate-level reader with enough introductory knowledge so that he or she can not only read the literature and study the next level textbook but can also apply the theory to find optimal solutions in practice. No more is needed than the usual background of an undergraduate engineering, science, or mathematics program: namely calculus, differential equations, and numerical integration. Although finding optimal solutions for these problems is a complex process involving the calculus of variations, the authors carefully lay out step-by-step the most important theorems and concepts. Numerous examples are worked to demonstrate how to apply the theories to everything from classical problems (e.g., crossing a river in minimum time) to engineering problems (e.g., minimum-fuel launch of a satellite). Throughout the book use is made of the time-optimal launch of a satellite into orbit as an important case study with detailed analysis of two examples: launch from the Moon and launch from Earth. For launching into the field of optimal solutions, look no further!.
Text of Note
Parameter Optimization -- Optimal Control Theory -- The Euler-Lagrange Theorem -- Application of the Euler-Lagrange Theorem -- The Weierstrass Condition -- The Minimum Principle -- Some Applications -- Weierstrass-Erdmann Corner Conditions -- Bounded Control Problems -- General Theory of Optimal Rocket Trajectories.
SERIES
Title
Space technology library
TOPICAL NAME USED AS SUBJECT
Control theory
Mathematical optimization
Aerospace engineering
Engineering
Control
Ordinary Differential Equations
Applied and Technical Physics
Aerospace Technology and Astronautics
LIBRARY OF CONGRESS CLASSIFICATION
Class number
E-BOOK
PERSONAL NAME - SECONDARY RESPONSIBILITY
Longuski, Jim
Guzm?n, Jose J
Prussing, John E
ORIGINATING SOURCE
Country
ایران
ELECTRONIC LOCATION AND ACCESS
Host name
9781461489443.pdf
Access number
عادی
Compression information
عادی
Date and Hour of Consultation and Access
9781461489443.pdf
Electronic Format Type
متن
old catalog
e
BL
1
a
Y
