書誌事項

Spaceflight dynamics

William E. Wiesel

(McGraw-Hill series in aeronautical and aerospace engineering)

McGraw-Hill, c1997

2nd ed.

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注記

Includes bibliographical references and index

"International editions 1997"-- t.p. verso

内容説明・目次

内容説明

Designed for undergraduate courses in Spacecraft Dynamics and Orbital Mechanics, this new edition offers a three-dimensional treatment of dynamics discussions of rigid body dynamics, rocket trajectories, and the space environment. An expert in his field, author William E. Wiesel presents a wealth of information in an easy-to-understand manner without the daunting mathematical rigor of graduate texts. Reference is made to actual flight vehicles and satellites to give students background on the type of work currently being done in this field.

目次

1 Partial Dynamics2 The Two Body Problem3 Earth Satellite Operations4 Rigid Body Dynamics5 Satellite Attitude Dynamics6 Gyroscopic Instruments7 Rocket Performances8 Reentry Dynamics9 The Space Environment10 The Restricted Three Body Problem11 Interplanetary TrajectoriesAppendixesA Vectors and MatriciesB Linear SystemsC Astrodynamic Constants

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詳細情報

  • NII書誌ID(NCID)
    BA41383196
  • ISBN
    • 0070701105
  • LCCN
    96019168
  • 出版国コード
    us
  • タイトル言語コード
    eng
  • 本文言語コード
    eng
  • 出版地
    New York
  • ページ数/冊数
    xiv, 332 p.
  • 大きさ
    24 cm
  • 分類
  • 件名
  • 親書誌ID
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