Orbital and celestial mechanics
著者
書誌事項
Orbital and celestial mechanics
(Progress in astronautics and aeronautics, v. 177)
American Institute of Aeronautics and Astronautics, c1998
大学図書館所蔵 全11件
  青森
  岩手
  宮城
  秋田
  山形
  福島
  茨城
  栃木
  群馬
  埼玉
  千葉
  東京
  神奈川
  新潟
  富山
  石川
  福井
  山梨
  長野
  岐阜
  静岡
  愛知
  三重
  滋賀
  京都
  大阪
  兵庫
  奈良
  和歌山
  鳥取
  島根
  岡山
  広島
  山口
  徳島
  香川
  愛媛
  高知
  福岡
  佐賀
  長崎
  熊本
  大分
  宮崎
  鹿児島
  沖縄
  韓国
  中国
  タイ
  イギリス
  ドイツ
  スイス
  フランス
  ベルギー
  オランダ
  スウェーデン
  ノルウェー
  アメリカ
内容説明・目次
内容説明
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.
目次
- 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.
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