| dc.contributor.author | Şahin, Merve | |
| dc.contributor.author | Cihan, Melahat | |
| dc.contributor.author | Kaya, Metin Orhan | |
| dc.contributor.editor | Hacioglu, A | |
| dc.contributor.editor | Ince, F | |
| dc.contributor.editor | Kaynak, O | |
| dc.date.accessioned | 2019-10-22T20:06:57Z | |
| dc.date.available | 2019-10-22T20:06:57Z | |
| dc.date.issued | 2015 | |
| dc.identifier.isbn | 978-1-4799-7697-3 | |
| dc.identifier.uri | https://hdl.handle.net/11421/22142 | |
| dc.identifier.uri | https://dx.doi.org/10.1109/RAST.2015.7208389 | en_US |
| dc.description | 7th International Conference on Recent Advances in Space Technologies (RAST) -- JUN 16-19, 2015 -- Istanbul, TURKEY | en_US |
| dc.description | WOS: 000381627000075 | en_US |
| dc.description.abstract | This paper contains calculations about propellant slosh for an upper stage rocket. The liquid fuel is modeled by using an equivalent mechanical model, from this point of view the stability of this rocket is examined by means of mass-spring model. In theory, a nonlinear mathematical model is derived and nonlinear feedback control laws are used. Specifications of the Attitude Vernier Upper Module (AVUM) upper stage rocket Vega are chosen for simulations. The results of this study are obtained for first four slosh modes. | en_US |
| dc.description.sponsorship | IEEE, AIAA, URSI, AESS, GRSS, EARSeL, ISPRS, Turkish Air Force Acad, Istanbul Tech Univ, Bogazici Univ, Middle E Tech Univ, Yildiz Tech Univ, Roketsan, Havelsan, Turksat, Aselsan, TAI, Tusas Engine Ind Inc, Petlas, ALP Havacilik, Mitsubishi Elect, Space & Defence Technologies, ThalesAlenia Space, Savunma Havacilik, MSI | en_US |
| dc.language.iso | eng | en_US |
| dc.publisher | IEEE | en_US |
| dc.relation.isversionof | 10.1109/RAST.2015.7208389 | en_US |
| dc.rights | info:eu-repo/semantics/closedAccess | en_US |
| dc.subject | Propellant Slosh | en_US |
| dc.subject | Equivalent Mechanical Model | en_US |
| dc.subject | Nonlinear Dynamics | en_US |
| dc.subject | Lagrange Equations | en_US |
| dc.title | Model and Control Problem for Space Vehicles with Propellant Slosh | en_US |
| dc.type | conferenceObject | en_US |
| dc.relation.journal | 2015 7th International Conference On Recent Advances in Space Technologies (Rast) | en_US |
| dc.contributor.department | Anadolu Üniversitesi, Sivil Havacılık Araştırma ve Uygulama Merkezi | en_US |
| dc.identifier.startpage | 461 | en_US |
| dc.identifier.endpage | 466 | en_US |
| dc.relation.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US] |
