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Improved Shaping Approach to the Preliminary Design of Low-Thrust Trajectories

Author
NOVAK, D. M1 ; VASILE, M2
[1] University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom
[2] University of Strathclyde, Glasgow, Scotland G1 1XQ, United Kingdom
Source

Journal of guidance, control, and dynamics. 2011, Vol 34, Num 1, pp 128-147, 20 p ; ref : 19 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)
Application spatiale Astéroïde Commande LQ Commande boucle fermée Contrainte Coordonnée sphérique Dynamique solide Méthode collocation Méthode directe Méthode domaine temps Méthode temps vol Rétroaction Spationef Trajectoire optimale
Keyword (en)
Space application Asteroid LQ control Closed feedback Constraint Spherical coordinate Solid dynamic Collocation method Direct method Time domain method Time of flight method Feedback regulation Spacecraft Optimal trajectory
Keyword (es)
Aplicación espacial Asteroide Control LQ Bucle realimentación cerrada Coacción Coordenada esférica Dinàmico sólido Método colocación Método directo Método dominio tiempo Método tiempo vuelo Retroacción Vehículo espacial Trayectoria óptima
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)

Discipline
Astronomy Physics : solid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
23739935

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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