Orbital Targeting Using Reduced Eccentric Anomaly Low-Thrust Coefficients
- Author
- HUDSON, Jennifer S1 ; SCHEERES, Daniel J2
[1] University of Michigan, Ann Arbor, Michigan 48019, United States
[2] University of Colorado, Boulder, Colorado 80309, United States - Source
Journal of guidance, control, and dynamics. 2011, Vol 34, Num 3, pp 820-831, 12 p ; ref : 28 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)
- Anomalie Commande mouvement Commande optimale Dynamique solide Elément orbital Equation variationnelle Excentricité Fonction coût Méthode moyenne Orbite transfert Poussée Programme commande Spationef Série Fourier
- Keyword (en)
- Anomaly Motion control Optimal control Solid dynamic Orbital elements Variational equation Eccentricity Cost function Averaging method Transfer orbit Thrust Control program Spacecraft Fourier series
- Keyword (es)
- Anomalía Dinàmico sólido Ecuación variacional Función coste Método medio Orbita transferida Empujón Programa mando Vehículo espacial
- 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 / 001D Applied sciences / 001D02 Computer science; control theory; systems / 001D02D Control theory. Systems / 001D02D07 Control system synthesis
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D02 Computer science; control theory; systems / 001D02D Control theory. Systems / 001D02D08 Optimal control
- 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 Physics : solid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 24186632
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
10.2514/1.51336 
https://dx.doi.org/10.2514/1.51336
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