Grant number: | 08/04999-4 |
Support Opportunities: | Regular Research Grants |
Start date: | August 01, 2008 |
End date: | July 31, 2010 |
Field of knowledge: | Engineering - Aerospace Engineering - Flight Dynamics |
Principal Investigator: | Antônio Fernando Bertachini de Almeida Prado |
Grantee: | Antônio Fernando Bertachini de Almeida Prado |
Host Institution: | Instituto Nacional de Pesquisas Espaciais (INPE). Ministério da Ciência, Tecnologia e Inovação (Brasil). São José dos Campos , SP, Brazil |
Abstract
The goal of this project is to continue the study of models and methods more used for the calculation of optimal space trajectories, from th epoint of view of minimizing the fual consumption, for a tarnsfer of a spacecraft between two given orbits. Several options will be studied for the dynamics, action of the control and optimization methods. Classical methods (Hohmann transfer, bi-eliptical, etc) and modern methods (gravitational capture and swing-by will also be studied. (AU)
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