Ozan Tekinalp

E-mail
tekinalp@metu.edu.tr
Department
Department of Aerospace Engineering
Scopus Author ID
Web of Science Researcher ID
Orbit Control of an Earth Orbiting Solar Sail Satellite
Polat, Halis Can; Tekinalp, Ozan (2022-09-01)
A concept for the utilization of solar sail satellite's propellant-free thrust capability at Low earth orbit (LEO) is proposed and its orbit control strategy is analyzed. Thrust vector control of the sail's normal directio...
BATCH ORBIT DETERMINATION COMPARISON FOR GEOSTATIONARY SATELLITES
KÖKER, ABDULKADİR; AYDIN, SEDA; DAĞ, ENES; YILMAZ, ÜMİT CEZMİ; Tekinalp, Ozan (2021-06-25)
Long term and safe relative orbit design for heterogeneous spacecraft clusters
Yaglioglu, Burak; Tekinalp, Ozan (2021-06-01)
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 ...
Airborne Wind Energy: Trajectory Tracking Controller Design of a Tethered Aircraft
Önen, Anıl Sami; Tekinalp, Ozan (2021-05-26)
Airborne wind energy has been intensely studied by the researchers, especially in the last decade(Ahrens, Diehl and Schmehl, 2014). It stems from the crosswind flight concept that was originallyintroduced by Loyd (1980). T...
Maneuver Planning Strategy for Rapid Response Solar Sail Satellite Concept
Polat, Halis Can; Tekinalp, Ozan (2021-01-11)
Regarding the use of Solar Sail Satellites at low altitudes for the proposed concept, a study is carried out to determine the critical mode switching altitude of the mission orbit and a review is presented for the non-id...
Sequential Orbit Determination Verification for Geostationary Satellites
KÖKER, ABDULKADİR; Tekinalp, Ozan; YILMAZ, ÜMİT CEZMİ; ŞAKACI, CEMAL (2021-01-01)
MISSION ANALYSIS OF A NEW SOLAR SAIL SATELLITE CONCEPT AT LOW EARTH ORBIT
Polat, Hakkı; Tekinalp, Ozan (2021-01-01)
© 2021, Univelt Inc. All rights reserved.Exploiting the propellant free maneuver capability of solar sail satellites for high resolution Earth observation mission is addressed with an elliptical low Earth orbit. The employ...
SEQUENTIAL ORBIT DETERMINATION VERIFICATION FOR GEOSTATIONARY SATELLITES
Köker, Abdulkadir; Tekinalp, Ozan; Yılmaz, Ü. Cezmi; Şakacı, Cemal (2021-01-01)
© 2021, Univelt Inc. All rights reserved.Sequential orbit determination using angle and range measurements for geostationary satellites is presented. The approach includes position, velocity and bias estimation with Unscen...
Mission Analysis of a New Solar Sail Satellite Concept at Low Earth Orbit
POLAT, HALİS CAN; Tekinalp, Ozan (2021-01-01)
Maneuver planning strategy for rapid response solar sail satellite concept
Polat, Halim; Tekinalp, Ozan (2021-01-01)
Regarding the use of Solar Sail Satellites at low altitudes for the proposed concept, a study is carried out to determine the critical mode switching altitude of the mission orbit and a review is presented for the non-idea...
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