Orbital and celestial mechanics
Author(s)
Bibliographic Information
Orbital and celestial mechanics
(Progress in astronautics and aeronautics, v. 177)
American Institute of Aeronautics and Astronautics, c1998
Available at 11 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
Orbital and Celestial Mechanics affords engineering students, professors and researchers alike an opportunity to cultivate the mathematical techniques necessary for this discipline - as well as physics and trajectory mechanics - using the familiar and universal concepts of classical physics. For nonspecialists and students unfamiliar with some of the underlying maths principles, the Vinti Spheroidal Method demonstrates computer routines for accurately calculating satellite orbit and ballistic trajectory. More than 20 years ago, Dr. Vinti's revolutionary method was used aboard a ballistic missile targeting programme with great success. His work continues to enable both students and professionals to predict position and velocity vectors for satellites and ballistic missiles almost as accurately as numerical integration. Now the best Vinti algorithms and companion computer source codes are available.
Table of Contents
- Newton's Laws
- The Two-Body Problem
- Lagrangian Dynamics
- The Hamiltonian Equations
- Canonical Transformations
- Hamilton-Jacobi Theory
- Hamilton-Jacobi Perturbation Theory
- The Vinti Spheroidal Method for Satellite Orbits and Ballistic Trajectories
- Delaunay Variables
- The Lagrange Planetary Equations
- The Planetary Disturbing Function
- Gaussian Variational Equations for the Jacobi Elements
- Gaussian Variational Equations for the Keplerian Elements
- Potential Theory
- The Gravitational Potential for a Planet
- Elementary Theory of Satellite Orbits with Use of the Mean Anomaly
- Elementary Theory of Satellite Orbits with Use of the True Anomaly
- The Effects of Drag on Satellite Orbits
- The Brouwer-von Zeipel Method 1
- The Brouwer-von Zeipel Method 2
- Lagrange and Poisson Brackets
- Lie Series
- Perturbations by Lie Series
- The General Three-Body Problem
- The Restricted Three-Body Problem
- Staeckel Systems. Appendices: Coordinate System and Coordinate Transformations
- Vinti Spheroidal Method Computational Procedure and Trajectory Propagators
- Examples
- How to Use the Vinti Routines.
by "Nielsen BookData"