Name: Fundamentals of Spacecraft Attitude Determination and Control (Space Technology Library) (en Inglés)
Price: 210420.00 CLP
Availability: InStock
Author: Markley, F. Landis ; Crassidis, John L.
ISBN: 9781493908011

portada Fundamentals of Spacecraft Attitude Determination and Control (Space Technology Library) (en Inglés)

Formato

Libro Físico

Autor

F. Landis Markley

John L. Crassidis

Editorial

Springer

Año

2014

Idioma

Inglés

N° páginas

486

Encuadernación

Tapa Dura

Dimensiones

23.4 x 15.6 x 2.7 cm

Peso

0.88 kg.

ISBN13

9781493908011

N° edición

2014

Categorías

Cálculo y análisis matemático
Ingeniería de control automático
Tecnología aeroespacial y aeronáutica
Astronáutica

Fundamentals of Spacecraft Attitude Determination and Control (Space Technology Library) (en Inglés)

F. Landis Markley (Autor) · John L. Crassidis (Autor) · Springer · Tapa Dura

Libro Nuevo

$ 210.420

$ 292.250

Ahorras: $ 81.830

28% descuento

Envío normal

Origen: Estados Unidos (Costos de importación incluídos en el precio)

Se enviará desde nuestra bodega entre el Lunes 06 de Mayo y el Miércoles 15 de Mayo.

Lo recibirás en cualquier lugar de Chile entre 1 y 3 días hábiles luego del envío.

Reseña del libro "Fundamentals of Spacecraft Attitude Determination and Control (Space Technology Library) (en Inglés)"

This book explores topics that are central to the field of spacecraft attitude determination and control. The authors provide rigorous theoretical derivations of significant algorithms accompanied by a generous amount of qualitative discussions of the subject matter. The book documents the development of the important concepts and methods in a manner accessible to practicing engineers, graduate-level engineering students and applied mathematicians. It includes detailed examples from actual mission designs to help ease the transition from theory to practice and also provides prototype algorithms that are readily available on the author's website.Subject matter includes both theoretical derivations and practical implementation of spacecraft attitude determination and control systems. It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion. This title also provides a thorough treatise of attitude dynamics including Jacobian elliptical functions. It is the first known book to provide detailed derivations and explanations of state attitude determination and gives readers real-world examples from actual working spacecraft missions. The subject matter is chosen to fill the void of existing textbooks and treatises, especially in state and dynamics attitude determination. MATLAB code of all examples will be provided through an external website.