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...
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 ...
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...
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...
Quaternion-based nonlinear attitude control of quadrotor formations carrying a slung load
Ariyibi, Segun O.; Tekinalp, Ozan (Elsevier BV, 2020-10-01)
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 l...
Fırdöndü uydular için sözle ölçümler kullanarak yönelim bağımsız gerçek zamanlı manyetometre kalibrasyonu
Çetin, Mustafa Efe; Söken, Halil Ersin; Tekinalp, Ozan (2020-09-09)
Küçük uydularda yönelim belirleme filtresinin kamera tabanlı ölçümler ile desteklenmesi
Güzel, Mehmet Burak; Söken, Halil Ersin; Tekinalp, Ozan (2020-09-09)
Oscillating Control Moment Gyroscope Mathematical Model Development, Verification and Results
Akbulut, Burak; Arberkli, Ferhat; Azgın, Kıvanç; Tekinalp, Ozan (null; 2020-02-15)
Imaging-based attitude determination algorithm for small satellites: Design and the preliminary results
Güzel, Mehmet Burak; Söken, Halil Ersin; Tekinalp, Ozan (2020-01-01)
Limitations for small satellite missions encourages researchers and engineers to use on-board equipment for multiple tasks. Thus, both space can be saved and the equipment redundancy can be prevented. For Earth-imaging sat...
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