Analytic Methods of Orbit Prediction and Control
Low-Thrust and Impulsive Propulsion Applications
Published on 11. April 2023
Book
Hardback
344 pages
978-1-62410-697-2 (ISBN)
Description
In this book, analytic methods of orbit prediction and control are investigated for important low-thrust and impulsive orbit change and station-keeping applications, and the results compared with actual exact numerically-integrated counterparts to evaluate their accuracy and applicability. With one eye on future autonomous on-orbit navigation applications both in near-circular and general elliptic orbit, with minimal computational effort and high accuracy, the orbit prediction and control segments of such autonomous navigation systems are explored by also taking into account the shadowing effect where no thrust is allowed, such as for electric propulsion applications. This book shows that many of these orbit prediction and station-keeping problems can be solved entirely in analytic form with very high accuracy, and allow the practitioners to solve similar problems by tailoring them to their own applications, and to better understand and evaluate the pertinent variables and parameters that drive and influence the resulting description and evolution of the orbits.
More details
Language
English
Place of publication
Reston
United States
Target group
Professional and scholarly
Dimensions
Height: 229 mm
Width: 152 mm
ISBN-13
978-1-62410-697-2 (9781624106972)
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Schweitzer Classification
Person
Jean Albert Kéchichian is a retired engineering specialist for The Aerospace Corporation. He has made lasting contributions in astronautical guidance and astrodynamics over the past 25 years. His extensive involvement in NASA's interplanetary and planetary missions include the design of the orbit sustenance maneuvering strategies of the TOPEX spacecraft, the design of the turn and orbit change maneuvers of the Active Magnetospheric Particle Tracer Explorers (AMPTE), direct support of the Pioneer Venus Orbiter mission operations, and the Galileo Probe trajectory reconstruction accuracy analysis. His software has been used by The Aerospace Corporation to fly actual spacecraft to the GEO orbit using optimal low-thrust transfer trajectories.
Dr. Kéchichian received his Engineer's degree in Aeronautical Engineering from the Universite de Liege in Wallonie, Belgium in 1971, and his MS in Mechanical Engineering from the University of California at Berkeley in 1976. In 1977, he received his PhD in Aeronautics and Astronautics from Stanford University. From 1979 to 1987, Dr. Kéchichian was a Maneuver and Orbit Determination Analyst at JPL. From 1987 to 1989 he worked as a Senior Engineering Specialist at Ford Aerospace. Dr. Kéchichian then worked as an Engineering Specialist at The Aerospace Corporation from 1989 until his retirement. He is also the author of Applied Nonsingular Astrodynamics, Cambridge University Press (2018) and Orbital Relative Motion and Terminal Rendezvous, Springer (2021).
Dr. Kéchichian received his Engineer's degree in Aeronautical Engineering from the Universite de Liege in Wallonie, Belgium in 1971, and his MS in Mechanical Engineering from the University of California at Berkeley in 1976. In 1977, he received his PhD in Aeronautics and Astronautics from Stanford University. From 1979 to 1987, Dr. Kéchichian was a Maneuver and Orbit Determination Analyst at JPL. From 1987 to 1989 he worked as a Senior Engineering Specialist at Ford Aerospace. Dr. Kéchichian then worked as an Engineering Specialist at The Aerospace Corporation from 1989 until his retirement. He is also the author of Applied Nonsingular Astrodynamics, Cambridge University Press (2018) and Orbital Relative Motion and Terminal Rendezvous, Springer (2021).