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Periodic orbits with low-thrust propulsion in the restricted three-body problem

Author
MORIMOTO, Mutsuko1 ; YAMAKAWA, Hiroshi2 ; UESUGI, Kuninori2
[1] Graduate University for Advanced Studies, Sagamihara 229-8510, Japan
[2] Japan Aerospace Exploration Agency, Sagamihara 229-8510, Japan
Source

Journal of guidance, control, and dynamics. 2006, Vol 29, Num 5, pp 1131-1139, 9 p ; ref : 13 ref

CODEN
JGCODS
ISSN
0731-5090
Scientific domain
Aeronautics astronautics; Control theory, operational research; Mechanics acoustics; Transportation
Publisher
American Institute of Aeronautics and Astronautics, Reston, VA
Publication country
United States
Document type
Article
Language
English
Keyword (fr)
Equation mouvement Force centrifuge Force gravitationnelle Force volume Masse variable Mouvement plan Mouvement périodique Orbite basse Orbite périodique Point équilibre Poussée Régime hors équilibre Système 2 corps Système 3 corps
Keyword (en)
Equation of motion Centrifugal force Gravitational force Body force Variable mass Plane motion Periodic motion Low orbit Periodic orbit Equilibrium point Thrust Non equilibrium conditions Two body system Three body system
Keyword (es)
Ecuación movimiento Fuerza centrífuga Fuerza gravitacional Fuerza volumen Masa variable Movimiento plano Movimiento periódico Orbita baja Orbita periódica Punto equilibrio Empujón Régimen fuera equilibrio Sistema 2 cuerpos Sistema 3 cuerpos
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D02 Computer science; control theory; systems / 001D02D Control theory. Systems / 001D02D13 Miscellaneous

Pascal
001 Exact sciences and technology / 001E Earth, ocean, space / 001E03 Astronomy / 001E03A Fundamental astronomy and astrophysics. Instrumentation, techniques, and astronomical observations / 001E03A10 Fundamental astronomy / 001E03A10E Orbit determination and improvement

Discipline
Astronomy Computer science : theoretical automation and systems
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
18120618

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

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