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Ozan Tekinalp

E-mail
tekinalp@metu.edu.tr
Department
Department of Aerospace Engineering
Scopus Author ID
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...
Slew Maneuver Control of Flexible Spacecraft
ALTINIŞIK, SÜLEYMAN; Tekinalp, Ozan (2019-07-04)
Passively Safe Relative Orbit Configurations over LongTime Intervals for Heterogeneously Distributed SpacecraftClusters
YAĞLIOĞLU, BURAK; Tekinalp, Ozan (2019-07-01)
Control of a Quadrotor Formation Carrying a Slung Load Using Flexible Bars
Tekinalp, Ozan; ARIYIBI, SEGUN (2019-06-17)
Safe Spacecraft Rendezvous Using Dual Quaternions on Time-Dependent Trajectories Generated by Model Predictive Control
Tekinalp, Ozan; BÜYÜKKOÇAK, ALİ TEVFİK (2019-01-07)
Oscillating Control Moment Gyroscope Experimental Results
AKBULUT, BURAK; ARBERKLİ, FERHAT; Azgın, Kıvanç; Tekinalp, Ozan (2019-01-07)
Formation Flight Design near Sun-Earth Collinear Libration Points under the Effect of Disturbances
Kutlu, Aykut; Tekinalp, Ozan (2019-01-01)
Solar Sail Application with a Proposed Low Earth Orbit Mission Concept
Polat, Halis Can; Tekinalp, Ozan (2019-01-01)
TRACKING CONTROL OF SPACECRAFT ATTITUDE AND POSITION ON TIME DEPENDENT TRAJECTORIES USING DUAL QUATERNIONS
BÜYÜKKOÇAK, ALİ TEVFİK; Tekinalp, Ozan (2019-01-01)
A spacecraft attitude and position control algorithm that uses dual quaternions for parametrization is proposed. Error dual quaternion and its derivative are obtained from the desired attitude and position information whic...
SAFE SPACECRAFT RENDEZVOUS WITH CONSTRAINED MODEL PREDICTIVE CONTROL
BÜYÜKKOÇAK, ALİ TEVFİK; Tekinalp, Ozan (2019-01-01)
Rendezvous and docking problem of a pair of low Earth orbit spacecraft is addressed. Equations for the nonlinear orbital relative motion of spacecraft are derived and a simulation code for this motion is developed. For the...