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1. Identity statement
Reference TypeBook Section
Sitemtc-m16.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositorysid.inpe.br/marciana/2004/09.14.08.56
Last Update2004:09.15.03.00.00 (UTC) administrator
Metadata Repositorysid.inpe.br/marciana/2004/09.14.08.56.03
Metadata Last Update2021:02.11.18.09.27 (UTC) administrator
Secondary KeyINPE-11285-PRE/6722
ISBN/ISSN85-17-00012-9
Citation KeyRoccoPradSouz:2004:CoTwMe
TitleComparison between two methods of optimal coplanar orbital transfers with time limit.
ProjectDinâmica orbital
Year2004
Access Date2024, May 16
Secondary TypePRE LI
Number of Files1
Size554 KiB
2. Context
Author1 Rocco, Evandro Marconi
2 Prado, Antonio Fernando Bertachini de Almeida
3 Souza, Marcelo Lopes de Oliveira e
Resume Identifier1 8JMKD3MGP5W/3C9JH37
2 8JMKD3MGP5W/3C9JGJA
3 8JMKD3MGP5W/3C9JHP4
Group1 DMC-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais. Divisão de Mecânica Espacial e Controle (INPE.DMC)
EditorKuga, Hélio Koiti
e-Mail Addressevandro@dem.inpe.br
Book TitleAdvances in space dynamics 4: celestial mechanics and astronautics
PublisherINPE
CitySão José dos Campos
Pages65-74
History (UTC)2005-07-25 14:06:02 :: jefferson -> administrator ::
2021-02-11 18:09:27 :: administrator -> marciana :: 2004
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
KeywordsSPACE MECHANICS AND CONTROL
Orbital dynamics
Transfer orbits
Elliptical orbits
Fuel consumption
Orbital maneuvers
MECÂNICA ESPACIAL E CONTROLE
Dinâmica orbital
Transferência de orbitas
Órbita elíptica
Consumo de combustível
Manobras orbitais
AbstractIn this work, we consider the problem of two-impulse orbital transfers between coplanar elliptical orbits with minimum fuel consumption but with a time limit for this transfer. This time limit imposes a new characteristic to the problem that rules out the majority of transfer methods available in the literature. Then, as a first method (Rocco1, Rocco et al.2), we used the equations presented by Lawden3. Those equations furnishes the optimal transfer orbit with fixed time for this transfer, between two elliptical coplanar orbits considering fixed terminal points. We adapted the method to cases with free terminal points and solved those equations to develop a software for orbital maneuvers. As a second method (Rocco1, Rocco et al.4), we used the equations presented by Eckel and Vinh5, that provides the transfer orbit between non-coplanar elliptical orbits with minimum fuel and fixed time transfer; or minimum time transfer for a prescribed fuel consumption; considering free terminal points. But in this work we consider only the problem with fixed time transfer, the case of minimum time for a prescribed fuel consumption was already studied in Rocco et al.6 Then, we modified the method to consider cases of coplanar orbital transfer, and develop a software for orbital maneuvers. Therefore, we have two software that solve the same problem using different methods. The first method uses the primer vector theory. The second method uses the ordinary theory of maxima and minima. So, to test the methods we choose the same terminal orbits and the same time as input. We could verify that we didn't obtain exactly the same result. Therefore, comparing and testing the results we could select the best method to solve the problem of coplanar orbital transfer with time limit.
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/sid.inpe.br/marciana/2004/09.14.08.56
zipped data URLhttp://urlib.net/zip/sid.inpe.br/marciana/2004/09.14.08.56
Languageen
Target FileComparison between.pdf
User Groupadministrator
jefferson
Visibilityshown
Copy HolderSID/SCD
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 3
sid.inpe.br/mtc-m21/2012/07.13.14.45.41 2
sid.inpe.br/mtc-m21/2012/07.13.14.54.38 2
DisseminationNTRSNASA, BNDEPOSITOLEGAL.
Host Collectionsid.inpe.br/banon/2003/08.15.17.40
6. Notes
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