Zobrazeno 1 - 10
of 75
pro vyhledávání: '"Ozan Tekinalp"'
Autor:
Halis Can Polat, Ozan Tekinalp
Publikováno v:
International Journal of Aeronautical and Space Sciences. 24:274-283
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::34eb5fa224bc569bcf40f0454a79fddc
https://doi.org/10.1007/s42405-022-00522-y
https://doi.org/10.1007/s42405-022-00522-y
Autor:
Ozan Tekinalp, Burak Yaglioglu
Publikováno v:
Advances in Space Research. 67:3546-3558
The problem of obtaining long term relative orbit configurations for spacecraft clusters with realistic operational considerations such as safety, station keeping and inter-spacecraft distances is addressed. Two different approaches are developed for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a8c818a0cb2853868da9a9d628b5030b
https://doi.org/10.1016/j.asr.2020.06.035
https://doi.org/10.1016/j.asr.2020.06.035
Autor:
Ozan Tekinalp, Halis Can Polat
Publikováno v:
AIAA Scitech 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b1cf0ee15956129c9b3285c8984244dc
https://doi.org/10.2514/6.2021-0183
https://doi.org/10.2514/6.2021-0183
Autor:
Ozan Tekinalp, Segun Ariyibi
Publikováno v:
AIAA Aviation 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4def6386e95f933a7e6d33f2e9890a86
https://doi.org/10.2514/6.2019-3270
https://doi.org/10.2514/6.2019-3270
Autor:
Ozan Tekinalp, Halis Can Polat
Publikováno v:
2019 9th International Conference on Recent Advances in Space Technologies (RAST).
Solar Sail applications utilizing the advantages of propellant-free and theoretically infinite specific impulse are widely investigated, especially for interplanetary/interstellar and near-Earth asteroid missions and non-Keplerian orbit designs. Howe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::437f3db877db481dfdcacaa92e6e8248
https://doi.org/10.1109/rast.2019.8767818
https://doi.org/10.1109/rast.2019.8767818
Autor:
Ozan Tekinalp, Aykut Kutlu
Publikováno v:
2019 9th International Conference on Recent Advances in Space Technologies (RAST).
This manuscript presents a methodology for the design of formation flight near Sun-Earth collinear libration points L1 and L2 that are located approximately 1.5 million kilometers from the Earth. The circular restricted three body problem is used for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::34b645cb7ec3931f44f2b21113b93204
https://doi.org/10.1109/rast.2019.8767804
https://doi.org/10.1109/rast.2019.8767804
Publikováno v:
2019 9th International Conference on Recent Advances in Space Technologies (RAST).
Initiated in early 2015 and officially started by the end of 2016, Asia Pacific Space Cooperation Organization (APSCO) Student Small Satellite (SSS) program aims student and faculties training from Member States (Bangladesh, China, Iran, Mongolia, Pa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b4c4f260be67af3ac434a05a62b7b8db
https://doi.org/10.1109/rast.2019.8767467
https://doi.org/10.1109/rast.2019.8767467
Autor:
Ozan Tekinalp, Ali Tevfik Büyükkoçak
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aec7952f9391527622eb49c5af314986
https://doi.org/10.2514/6.2019-1914
https://doi.org/10.2514/6.2019-1914
Publikováno v:
Journal of Vibration and Control. 24:1239-1263
For output-feedback control of linear time-varying (LTV) and nonlinear systems, this paper focuses on control based on the forward propagating Riccati equation (FPRE). FPRE control uses dual difference (or differential) Riccati equations that are sol
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ab1358d4b9ef27bedee2dfd91902056c
https://doi.org/10.1177/1077546316655913
https://doi.org/10.1177/1077546316655913
Autor:
Segun Ariyibi, Ozan Tekinalp
Publikováno v:
Aerospace Science and Technology. 105:105995
Control of a pair of quadrotors carrying a slung load is addressed. A hierarchical control algorithm is implemented on the leader quadrotor. The control system features a linear quadratic tracking controller on its outer loop for velocity command tra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1ac21b731a3172b0a940087e07891c85
https://doi.org/10.1016/j.ast.2020.105995
https://doi.org/10.1016/j.ast.2020.105995