| Safe landing area determination for a moon lander by reachability analysis YE Arslantaş, T Oehlschlägel, M Sagliano Acta Astronautica 128, 607-615, 2016 | 26 | 2016 |
| Spartan: an improved global pseudospectral algorithm for high-fidelity entry-descent-landing guidance analysis L Huneker, M Sagliano, Y Arslantas | 17 | 2015 |
| A comparison between advanced model-free PID and model-based LQI attitude control of a quadcopter using asynchronous android flight data MA Alsharif, YE Arslantas, MS Hölzel 2017 25th Mediterranean Conference on Control and Automation (MED), 1023-1028, 2017 | 14 | 2017 |
| Exact Hybrid Jacobian Computation for Optimal Trajectories via Dual Number Theory V D'Onofrio, M Sagliano, YE Arslantas AIAA Guidance, Navigation, and Control Conference, 0867, 2016 | 11 | 2016 |
| Approximation of attainable landing area of a moon lander by reachability analysis Y Arslantas, T Oehlschlägel, M Sagliano, S Theil, C Braxmaier | 7 | 2014 |
| Advanced pid attitude control of a quadcopter using asynchronous android flight data MA Alsharif, YE Arslantas, MS Hölzel 2017 International Conference on Unmanned Aircraft Systems (ICUAS), 1602-1607, 2017 | 6 | 2017 |
| Attainable landing area computation of a lunar lander with uncertainty by reachability Analysis YE Arslantas, S Theil Advances in Aerospace Guidance, Navigation and Control: Selected Papers of …, 2018 | 5 | 2018 |
| Real-time Capable Nonlinear Model Predictive Controller Design for The Upper Stage of a Launch Vehicle YE Arslantas, T Oehlschlägel TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES …, 2016 | 3 | 2016 |
| Development of a Reachability Analysis Algorithm for Space Applications Y Arslantas Universität Bremen, 2017 | 1 | 2017 |
| Attainable Landing Area Computation of Lunar Landers with Pseudo-Spectral and Polynomial Based Guidance Methods Y Arslantas, M Alsharif, M Hölzel, S Theil Proceedings of the International Astronautical Congress, IAC, 2017 | | 2017 |
