Numerical computation of optimal low-thrust limited-power trajectories - Transfers between coplanar circular orbits



Document title: Numerical computation of optimal low-thrust limited-power trajectories - Transfers between coplanar circular orbits
Journal: Journal of the Brazilian Society of Mechanical Sciences and Engineering
Database: PERIÓDICA
System number: 000312314
ISSN: 1678-5878
Authors: 1
2
Institutions: 1Instituto Tecnologico de Aeronautica, Departamento de Matematica, Sao Jose dos Campos, Sao Paulo. Brasil
2Centro Tecnico Aeroespacial, Sao Jose dos Campos, Sao Paulo. Brasil
Year:
Season: Abr-Jun
Volumen: 27
Number: 2
Pages: 178-185
Country: Brasil
Language: Inglés
Document type: Artículo
Approach: Experimental
English abstract An algorithm based on gradient techniques, proposed in a companion paper, is applied to numerical analysis of optimal low-thrust limited-power trajectories for simple transfer (no rendezvous) between coplanar circular orbits in a central Newtonian gravity field. The proposed algorithm combines the main positive characteristics of two well-known methods in optimization of trajectories: the steepest-descent method and the direct second variation method. The analysis is carried out for various radius ratios and transfer durations. The results are compared to the ones provided by a linear analytical theory. The performance of the proposed algorithm shows that it is a good tool in determining optimal low-thrust limited-power trajectories between close circular coplanar orbits in a Newtonian central gravity field
Disciplines: Matemáticas,
Ciencia y tecnología,
Ingeniería
Keyword: Trayectorias espaciales,
Algoritmos,
Cohetes,
Energía,
Propulsión
Keyword: Mathematics,
Science and technology,
Engineering,
Propulsion,
Space trajectories,
Power,
Algorithms,
Rockets
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