Muutke küpsiste eelistusi

Algorithms for Satellite Orbital Dynamics 2023 ed. [Pehme köide]

Translated by ,
  • Formaat: Paperback / softback, 553 pages, kõrgus x laius: 235x155 mm, 63 Illustrations, black and white; XXXI, 553 p. 63 illus., 1 Paperback / softback
  • Sari: Springer Series in Astrophysics and Cosmology
  • Ilmumisaeg: 22-Jun-2024
  • Kirjastus: Springer Verlag, Singapore
  • ISBN-10: 9811948410
  • ISBN-13: 9789811948411
  • Pehme köide
  • Hind: 62,59 €*
  • * hind on lõplik, st. muud allahindlused enam ei rakendu
  • Tavahind: 73,64 €
  • Säästad 15%
  • Raamatu kohalejõudmiseks kirjastusest kulub orienteeruvalt 2-4 nädalat
  • Kogus:
  • Lisa ostukorvi
  • Tasuta tarne
  • Tellimisaeg 2-4 nädalat
  • Lisa soovinimekirja
  • Formaat: Paperback / softback, 553 pages, kõrgus x laius: 235x155 mm, 63 Illustrations, black and white; XXXI, 553 p. 63 illus., 1 Paperback / softback
  • Sari: Springer Series in Astrophysics and Cosmology
  • Ilmumisaeg: 22-Jun-2024
  • Kirjastus: Springer Verlag, Singapore
  • ISBN-10: 9811948410
  • ISBN-13: 9789811948411
This book highlights the fundamental physics of orbit theory, dynamical models, methods of orbit determination, design, measurement, adjustment, and complete calculations for the position, tracking, and prediction of satellites and deep spacecraft.

This book highlights the fundamental physics of orbit theory, dynamical models, methods of orbit determination, design, measurement, adjustment, and complete calculations for the position, tracking, and prediction of satellites and deep spacecraft. It emphasizes specific methods, related mathematical calculations, and worked examples and exercises. Therefore, technicians and engineers in the aerospace industry can directly apply them to their practical work. Dedicated to undergraduate students and graduate students, researchers, and professionals in astronomy, physics, space science, and related aerospace industries, the book is an integrated work based on the accumulated knowledge in satellite orbit dynamics and the author’s more than five decades of personal research and teaching experience in astronomy and aerospace dynamics.
Preface.- Introduction.- Chapter 1 Selection and Conversions of
Coordinate System.- Chapter 2 Complete Solutions of the two-body
Problem.- Chapter 3 Analytical methods of structural solutions for a
perturbed satellite orbit.- Chapter 4 Non-singular point analytical solutions
for a perturbed Earths satellite orbit by extrapolation.- Chapter 5 Design
of satellite orbit and lifespan estimation.- Chapter 6 Orbital solutions of
satellites of the Moon and major planets.- Chapter 7 Orbits in the restricted
three-body problem and calculation methods.- Chapter 8 Numerical methods for
satellite orbit extrapolation.- Chapter 9 Formulation of orbit determination
and calculation of initial orbit.- Chapter 10 Determination of precession
orbit.- Appendix.
Author: Dr. Lin LIU Dr. Lin LIU is a distinguished professor at the Astronomy and Space Science Institute, Nanjing University. He is regarded as the main founder of the research in celestial dynamics and spacecraft orbit determination in China. He has been involved in Chinese Space projects including the Shenzhou Spacecraft project and the Moon Exploration project. He formerly held the director positions at the Chinese Astronomy Society and the Chinese Aerospace Society Translator: Dr. Shengpan Zhang Dr. Shengpan Zhang is a retired scientist. She formerly worked as an associate professor at Nanjing University and as a research scientist at York University, both in astronomy. She received NASAs Group Achievement Award for her contribution to the UARS space project. Her research focuses on the stability of the solar system and orbit theory, and the upper atmospheric physics.