Optimal Lunar Orbit Insertion from a Variable Symmetric Free-Return Trajectory
- Author
- JESICK, Mark1 ; OCAMPO, Cesar1
[1] University of Texas at Austin, Austin, Texas 78712, United States - Source
Journal of guidance, control, and dynamics. 2011, Vol 34, Num 6, pp 1867-1875, 9 p ; ref : 24 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)
- Dynamique solide Modélisation Mécanique céleste Méthode balistique Méthode séquentielle Optimisation Orbite Orientation Perturbation linéaire Programmation quadratique Solution exacte Système 3 corps Système n corps Technique perturbation
- Keyword (en)
- Solid dynamic Modelling Celestial mechanics Shooting method Sequential method Optimization Orbits Orientation Linear perturbation Quadratic programming Exact solution Three body system N body system Perturbation techniques
- Keyword (es)
- Dinàmico sólido Método balistico Método secuencial Perturbación lineal Solución exacta Sistema 3 cuerpos Sistema n cuerpos
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40F Solid mechanics / 001B40F10 Solid dynamics (ballistics, collision, multibody system, stabilization...)
- 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 / 001E03A10C Celestial mechanics (including n-body problems)
- 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 Physics : solid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 24720115
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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DOI
10.2514/1.53826 
https://dx.doi.org/10.2514/1.53826
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