Atilla Dogan, Ph.D.
Affiliations: | 2000 | University of Michigan, Ann Arbor, Ann Arbor, MI |
Area:
Aerospace EngineeringGoogle:
"Atilla Dogan"Parents
Sign in to add mentorPierre T. Kabamba | grad student | 2000 | University of Michigan | |
(Guidance strategies for microburst escape.) |
BETA: Related publications
See more...
Publications
You can help our author matching system! If you notice any publications incorrectly attributed to this author, please sign in and mark matches as correct or incorrect. |
Kartal Y, Kolaric P, Lopez V, et al. (2019) Backstepping approach for design of PID controller with guaranteed performance for micro-air UAV Control Theory and Technology. 18: 19-33 |
Okolo WA, Dogan A, Blake W. (2018) Ride Quality Within Conventional and Delta-Wing Trail Aircraft in Formation Flight Journal of Aircraft. 55: 1592-1604 |
Erturk SA, Dogan A. (2017) Dynamic Simulation and Control of Mass-Actuated Airplane Journal of Guidance Control and Dynamics. 40: 1939-1953 |
Okolo W, Dogan A, Blake W. (2015) Alternate trimming methods for trailing aircraft in formation flight Journal of Guidance, Control, and Dynamics. 38: 2018-2024 |
Sevil HE, Dogan A. (2015) Fault diagnosis in air data sensors for receiver aircraft in aerial refueling Journal of Guidance, Control, and Dynamics. 38: 1959-1975 |
Okolo W, Dogan A, Blake W. (2015) Effect of trail aircraft trim on optimum location in formation flight Journal of Aircraft. 52: 1201-1213 |
Dogan A, Blake W. (2014) Maneuverability of large receiver of different size and weight in Aerial Refueling Journal of Guidance, Control, and Dynamics. 37: 1880-1896 |
Dogan A, Blake W, Haag C. (2013) Bow Wave Effect in Aerial Refueling: Computational Analysis and Modeling Journal of Aircraft. 50: 1856-1868 |
Lee JH, Sevil HE, Dogan A, et al. (2013) Estimation of maneuvering aircraft states and time-varying wind with turbulence Aerospace Science and Technology |
Lee JH, Sevil HE, Dogan A, et al. (2012) Estimation of Receiver Aircraft States and Wind Vectors in Aerial Refueling Journal of Guidance Control and Dynamics. 37: 265-276 |