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Orbital relative motion and terminal...

Kechichian, Jean Albert.

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Orbital relative motion and terminal rendezvous = analytic and numerical methods for spaceflight guidance applications /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Orbital relative motion and terminal rendezvous/ by Jean Albert Kechichian.
Reminder of title:	analytic and numerical methods for spaceflight guidance applications /
Author:	Kechichian, Jean Albert.
Published:	Cham :Springer International Publishing : : 2021.,
Description:	xv, 417 p. :ill., digital ;24 cm.
[NT 15003449]:	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)
Contained By:	Springer Nature eBook
Subject:	Orbital transfer (Space flight) -
Online resource:	https://doi.org/10.1007/978-3-030-64657-8
ISBN:	9783030646578

Orbital relative motion and terminal rendezvous = analytic and numerical methods for spaceflight guidance applications /
Kechichian, Jean Albert.

Orbital relative motion and terminal rendezvousanalytic and numerical methods for spaceflight guidance applications /[electronic resource] :by Jean Albert Kechichian. - Cham :Springer International Publishing :2021. - xv, 417 p. :ill., digital ;24 cm. - Space technology library ;39. - Space technology library ;39..

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)

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.

ISBN: 9783030646578

Standard No.: 10.1007/978-3-030-64657-8doiSubjects--Topical Terms:

3298731
Orbital transfer (Space flight)

LC Class. No.: TL1075 / .K434 2021

Dewey Class. No.: 629.4113

Orbital relative motion and terminal rendezvous = analytic and numerical methods for spaceflight guidance applications /
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245 1 0 $a Orbital relative motion and terminal rendezvous $h [electronic resource] : $b analytic and numerical methods for spaceflight guidance applications / $c by Jean Albert Kechichian.
260 $a Cham : $b Springer International Publishing : $b Imprint: Springer, $c 2021.
300 $a xv, 417 p. : $b ill., digital ; $c 24 cm.
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505 0 $a 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 $a 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.
650 0 $a Orbital transfer (Space flight) $3 3298731
650 0 $a Trajectory optimization. $3 2059202
650 0 $a Orbital rendezvous (Space flight) $3 864618
650 0 $a Mathematical physics. $3 516853
650 1 4 $a Aerospace Technology and Astronautics. $3 928116
650 2 4 $a Astronomy, Astrophysics and Cosmology. $3 890823
650 2 4 $a Theoretical, Mathematical and Computational Physics. $3 1066859
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830 0 $a Space technology library ; $v 39. $3 3494266
856 4 0 $u https://doi.org/10.1007/978-3-030-64657-8
950 $a Engineering (SpringerNature-11647)