James M. Longuski, José J. Guzmán, John E. Prussing
مشخصات ظاهری
نام خاص و کميت اثر
1 online resource (xx, 273 pages) :
ساير جزييات
illustrations.
فروست
عنوان فروست
Space Technology Library
یادداشتهای مربوط به کتابنامه ، واژه نامه و نمایه های داخل اثر
متن يادداشت
Includes bibliographical references and index
یادداشتهای مربوط به مندرجات
متن يادداشت
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
بدون عنوان
0
یادداشتهای مربوط به خلاصه یا چکیده
متن يادداشت
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!
ویراست دیگر از اثر در قالب دیگر رسانه
شماره استاندارد بين المللي کتاب و موسيقي
9781461489443
موضوع (اسم عام یاعبارت اسمی عام)
موضوع مستند نشده
Aerospace engineering.
موضوع مستند نشده
Control theory.
موضوع مستند نشده
Mathematical optimization.
موضوع مستند نشده
Aerospace Technology and Astronautics.
موضوع مستند نشده
Applied and Technical Physics.
موضوع مستند نشده
Control.
موضوع مستند نشده
Engineering.
موضوع مستند نشده
Ordinary Differential Equations.
مقوله موضوعی
موضوع مستند نشده
TEC004000
موضوع مستند نشده
TJFM
رده بندی ديویی
شماره
515/
.
642
ويراست
23
رده بندی کنگره
شماره رده
QA402
.
3
نام شخص به منزله سر شناسه - (مسئولیت معنوی درجه اول )