Orbital Relative Motion and Terminal Rendezvous (Record no. 78155)

000 -LEADER
fixed length control field 04712nam a22005775i 4500
001 - CONTROL NUMBER
control field 978-3-030-64657-8
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801220045.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 210412s2021 sz | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783030646578
-- 978-3-030-64657-8
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
100 1# - AUTHOR NAME
Author Kéchichian, Jean Albert.
245 10 - TITLE STATEMENT
Title Orbital Relative Motion and Terminal Rendezvous
Sub Title Analytic and Numerical Methods for Spaceflight Guidance Applications /
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2021.
300 ## - PHYSICAL DESCRIPTION
Number of Pages XV, 417 p. 152 illus., 100 illus. in color.
490 1# - SERIES STATEMENT
Series statement Space Technology Library,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Chapter 1. The Second-Order Analytic Approximation to the Solution of the Euler-Hill Equations of Relative Motion -- Chapter 2. Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influence of the J2 and J3 Earth Zonal Harmonics, in Rotating and Inertial Cartesian Reference Frames -- Chapter 3. Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influence of the Luni-Solar Gravity, in Rotating and Inertial Cartesian Reference Frames -- Chapter 4. Effect of Luni-Solar Gravity Perturbations on a Near-Circular Orbit: Third-Body Orbit Eccentricity Considerations -- Chapter 5. Effect of Atmospheric Drag Perturbation on Circular Orbits: Atmosphere Rotation Considerations -- Chapter 6. Analytic Solution of Terminal Rendezvous in Near-Circular Orbit Around the Oblate Earth: The Computation of the Starting Guess for Iterations -- Chapter 7. Techniques of Accurate Analytic Terminal Rendezvous in Near-Circular Orbit -- Chapter 8. Coplanar Two-Impulse Rendezvous in General Elliptic Orbit with Drag -- Chapter 9. The Analysis of the Relative Motion in General Elliptic Orbit With Respect to a Dragging and Precessing Coordinate Frame -- Chapter 10. The Algorithm of the Two-Impulse Time-Fixed Noncoplanar Rendezvous with Drag and Oblateness Effects -- Chapter 11. The Analysis and Implementation of In-Plane Stationkeeping of Continuously Perturbed Walker Constellations -- Chapter 12. The Mathematical Models of the Jet Propulsion Laboratory (JPL) Artificial Satellite Analysis Program (ASAP).
520 ## - SUMMARY, ETC.
Summary, etc This book provides a comprehensive analysis of time-fixed terminal rendezvous around the Earth using chemical propulsion. The book has two main objectives. The first is to derive the mathematics of relative motion in near-circular orbit when subjected to perturbations emanating from the oblateness of the Earth, third-body gravity, and atmospheric drag. The mathematics are suitable for quick trajectory prediction and the creation of computer codes and efficient software to solve impulsive maneuvers and fly rendezvous missions. The second objective of this book is to show how the relative motion theory is applied to the exact precision-integrated, long-duration, time-fixed terminal rendezvous problem around the oblate Earth for the general elliptic orbit case. The contents are both theoretical and applied, with long-lasting value for aerospace engineers, trajectory designers, professors of orbital mechanics, and students at the graduate level and above. .
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-3-030-64657-8
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Cham :
-- Springer International Publishing :
-- Imprint: Springer,
-- 2021.
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-- text
-- txt
-- rdacontent
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-- computer
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-- rdamedia
338 ## -
-- online resource
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-- rdacarrier
347 ## -
-- text file
-- PDF
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650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Outer space—Exploration.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mathematical physics.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Space Exploration and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Theoretical, Mathematical and Computational Physics.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 2542-8896 ;
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-- ZDB-2-ENG
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-- ZDB-2-SXE

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