Ozan Tekinalp

Department of Aerospace Engineering
Scopus Author ID
Web of Science Researcher ID
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...
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...
Scatter and sensitivity analysis of a projectile modeled under magnus effect
Muhiddinoğlu, Alp; Yayla, Koray; Tekinalp, Ozan (null; 2019-09-18)
A mission analysis software for small satellites
Koprücü, Salih Ulaş; Özçelik, Salih Abdullah; Altunay, Şulenur; Yağlıoğlu, Burak; Tekinalp, Ozan (null; 2019-09-18)
In this paper, a mission analysis software is described for LEO small satellites which is developed by students participating in the APSCO (Asia-Pacific Space Cooperation Organization) Student Small Satellite (SSS) project...
Lateral-directional control of a highly maneuverable jet aircraft based on combination of modal and optimal control theory
Mesce, Volkan; Tekinalp, Ozan (null; 2019-09-18)
A feedback matrix is calculated to assign closed loop eigenvalues of the lateral-directional stability augmentation system of the aircraft with low closed loop eigenvalue sensitivity at minimum cost which guarantees +inf a...
Citation Formats