Switched-gain guidance for impact angle control under physical constraints R Tekin, KS Erer Journal of Guidance, Control, and Dynamics 38 (2), 205-216, 2015 | 147 | 2015 |
Polynomial shaping of the look angle for impact-time control R Tekin, KS Erer, F Holzapfel Journal of Guidance, Control, and Dynamics 40 (10), 2668-2673, 2017 | 111 | 2017 |
Impact time and angle control based on constrained optimal solutions KS Erer, R Tekin Journal of Guidance, Control, and Dynamics 39 (10), 2448-2454, 2016 | 92 | 2016 |
Adaptive impact time control via look-angle shaping under varying velocity R Tekin, KS Erer, F Holzapfel Journal of Guidance, Control, and Dynamics 40 (12), 3247-3255, 2017 | 75 | 2017 |
Control of impact time with increased robustness via feedback linearization R Tekin, KS Erer, F Holzapfel Journal of Guidance, Control, and Dynamics 39 (7), 1682-1689, 2016 | 75 | 2016 |
Look angle constrained impact angle control based on proportional navigation KS Erer, R Tekin, MK Ozgoren AIAA guidance, navigation, and control conference, 0091, 2015 | 58 | 2015 |
Impact time control with generalized-polynomial range formulation R Tekin, KS Erer, F Holzapfel Journal of Guidance, Control, and Dynamics 41 (5), 1190-1195, 2018 | 53 | 2018 |
Impact time and angle control against moving targets with look angle shaping R Tekin, KS Erer Journal of Guidance, Control, and Dynamics 43 (5), 1020-1025, 2020 | 43 | 2020 |
Generalized impact time and angle control via look-angle shaping S Kang, R Tekin, F Holzapfel Journal of Guidance, Control, and Dynamics 42 (3), 695-702, 2019 | 43 | 2019 |
Biased proportional navigation with exponentially decaying error for impact angle control and path following KS Erer, R Tekin, MK Özgören 2016 24th Mediterranean Conference on Control and Automation (MED), 238-243, 2016 | 26 | 2016 |
Modeling and Vertical Launch Analysis of an Aero-and Thrust Vector Controlled Surface to Air Missile R Tekin, Ö Atesoglu, K Leblebicioglu AIAA Atmospheric Flight Mechanics Conference, 7639, 2010 | 26 | 2010 |
MATLAB and LabVIEW in modeling, analysis and real time control of a motion control system R Tekin IEEE ICCA 2010, 2077-2081, 2010 | 18 | 2010 |
Impact vector guidance KS Erer, R Tekin Journal of Guidance, Control, and Dynamics 44 (10), 1892-1901, 2021 | 14 | 2021 |
Guaranteed smooth trajectory generation for field-of-view constrained impact-time control H Hong, R Tekin, F Holzapfel Journal of Guidance, Control, and Dynamics 44 (4), 898-904, 2021 | 13 | 2021 |
Design, modeling, guidance and control of a vertical launch surface to air missile R Tekin Middle East Technical University, 2010 | 9 | 2010 |
Quartic range shaping for impact time control R Tekin, KS Erer, F Holzapfel 2017 25th Mediterranean Conference on Control and Automation (MED), 1213-1218, 2017 | 8 | 2017 |
Impact angle control based on feedback linearization R Tekin, F Holzapfel AIAA Guidance, Navigation, and Control Conference, 1509, 2017 | 8 | 2017 |
Composite impact vector control based on Apollo descent guidance R TEKIN, MK Erer, KS,ÖZGÖREN Chinese Journal of Aeronautics 35 (7), 67-74, 2022 | 7 | 2022 |
Flight control algorithms for a vertical launch air defense missile R Tekin, O Atesoglu, K Leblebicioglu Advances in Aerospace Guidance, Navigation and Control: Selected Papers of …, 2013 | 6 | 2013 |
Considerations on Boost Phase Modeling and Guidance Command Generation R Tekin, KS Erer AIAA Guidance, Navigation, and Control Conference, Kissimee, FL BIOGRAPHY …, 2015 | 5 | 2015 |