• Epicyclic motion of satellites...

Treffer: Epicyclic motion of satellites about an oblate planet

Title:
Epicyclic motion of satellites about an oblate planet
Authors:
HASHIDA, Yoshikazu, PALMER, Philip L
Source:
Journal of guidance, control, and dynamics. 24(3):586-596
Publisher Information:
Reston, VA: American Institute of Aeronautics and Astronautics, 2001.
Publication Year:
2001
Physical Description:
print, 13 ref
Original Material:
CRAN
Subject Terms:
Aeronautics astronautics, Aéronautique, astronautique, Control theory, operational research, Automatique, recherche opérationnelle, Mechanics acoustics, Mécanique et acoustique, Transportation, Transports, Sciences exactes et technologie, Exact sciences and technology, Sciences appliquees, Applied sciences, Informatique; automatique theorique; systemes, Computer science; control theory; systems, Automatique théorique. Systèmes, Control theory. Systems, Modélisation et identification, Modelling and identification, Divers, Miscellaneous, Terre, ocean, espace, Earth, ocean, space, Astronomie, Astronomy, Astronomie fondamentale et astrophysique. Instrumentation, techniques, et observations astronomiques, Fundamental astronomy and astrophysics. Instrumentation, techniques, and astronomical observations, Techniques d'observation et de réduction des données. Simulation et modélisation par ordinateur, Observation and data reduction techniques. Computer modeling and simulation, Méthodes mathématiques et méthodes de simulation sur ordinateur, Mathematical procedures and computer techniques, Configuration symétrie axiale, Axisymmetric configuration, Configuración simétrica axial, Durabilité, Durability, Durabilidad, Durée vie, Lifetime, Modèle géométrique, Geometrical model, Modelo geométrico, Modélisation, Modelling, Mouvement, Motion, Orbite, Orbits, Ordre 2, Second order, Orden 2, Potentiel, Potentials, Réponse temporelle, Time response, Respuesta temporal, Satellite, Satellites, Symétrie axiale, Axial symmetry
Document Type:
Fachzeitschrift Article
File Description:
text
Language:
English
Author Affiliations:
University of Surrey, Guildford, GU2 7XH, United Kingdom
ISSN:
0731-5090
Access URL:
http://pascal-francis.inist.fr/vibad/index.php?action=search&terms=5683478
Rights:
CC BY 4.0
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
Notes:
Astronomy

Computer science; theoretical automation; systems
Accession Number:
edscal.5683478
Database:
PASCAL Archive

Weitere Informationen

An analytic formulation is presented of a near circular orbit of a satellite about an axisymmetric potential. The model has a simple analytic form that is capable of describing all of the gravitational perturbative effects. Unlike more rigorous treatments, our approach has a simple geometric interpretation and greater mathematical simplicity than conventional descriptions of the perturbed motion, yet is sufficiently accurate to describe the motion of a satellite over its lifetime. The formulation of the orbit, based on epicyclic motion, is presented, and how all of the terms in the geopotential can be incorporated into the same formulation is demonstrated. Also considered are second-order effects arising from the J2 term, which provides sufficient accuracy in the modeling for most satellite applications. Some simulation results are presented to establish the accuracy of the predictive model over time.