An introduction to the mathematics and methods of astrodynamics
Author(s)
Bibliographic Information
An introduction to the mathematics and methods of astrodynamics
(AIAA education series)
American Institute of Aeronautics and Astronautics, c1999
Rev. ed
Available at 20 libraries
  Aomori
  Iwate
  Miyagi
  Akita
  Yamagata
  Fukushima
  Ibaraki
  Tochigi
  Gunma
  Saitama
  Chiba
  Tokyo
  Kanagawa
  Niigata
  Toyama
  Ishikawa
  Fukui
  Yamanashi
  Nagano
  Gifu
  Shizuoka
  Aichi
  Mie
  Shiga
  Kyoto
  Osaka
  Hyogo
  Nara
  Wakayama
  Tottori
  Shimane
  Okayama
  Hiroshima
  Yamaguchi
  Tokushima
  Kagawa
  Ehime
  Kochi
  Fukuoka
  Saga
  Nagasaki
  Kumamoto
  Oita
  Miyazaki
  Kagoshima
  Okinawa
  Korea
  China
  Thailand
  United Kingdom
  Germany
  Switzerland
  France
  Belgium
  Netherlands
  Sweden
  Norway
  United States of America
Description and Table of Contents
Description
This comprehensive text documents the fundamental theoretical developments in astrodynamics and space navigation that led to Man's ventures into space. It includes the essential elements of celestial mechanics, spacecraft trajectories, and space navigation, as well as the history of the underlying mathematical developments. The material presented in the text represents a 25-year evolution in course material by Dr Battin. Former students who benefitted from this material include three of the astronauts who walked on the moon. The text format offers flexibility for the user. Chapters are largely independent of each other and may be read or taught in any order, offering the opportunity to organize an undergraduate or graduate course that meets the needs of students having various levels of background and preparation. Further, the book covers more subject matter than is covered in a single course of instruction, thereby motivating students to stray from the beaten path of the classroom.
Table of Contents
- Part 1 Hypergeometric Functions and Elliptic Integrals: Some Basic Topics In Analytical Dynamics
- The Problem of Two Bodies
- Two-Body Orbits and the Initial-Value Problem
- Solving Kepler's Equation
- Two-Body Orbital Boundary Value Problem
- Solving Lambert's Problem
- Appendices. Part 2 Non-Keplerian Motion: Patched-Conic Orbits and Perturbation Methods
- Variation of Parameters
- Two-Body Orbital Transfer
- Numerical Integration of Differential Equations
- The Celestial Position Fix
- Space Navigation
- Appendices.
by "Nielsen BookData"