2020
Flight simulation assessment of autorotation algorithms and cues (Conference Paper)
Alam, M., Jump, M., Eberle, B., & Rogers, J. (2020). Flight simulation assessment of autorotation algorithms and cues. In Vertical Flight Society's 76th Annual Forum and Technology Display.
2019
Alam, M. M., Jump, M., & Cameron, N. (2019). Can Time-To-Contact Be Used To Model A Helicopter Autorotation?. In Asian/Australian Rotorcraft Forum (pp. 1-7). Ankara, Turkey.
Alam, M., & Hromcik, M. (2019). Structural load alleviation using distributed delay shaper: Application to flexible aircraft. Control Engineering Practice, 89, 130-142. doi:10.1016/j.conengprac.2019.05.005DOI: 10.1016/j.conengprac.2019.05.005
2018
Jump, M., Alam, M., Cameron, N., Fell, T., Rogers, J., Eberle, B., . . . Repola, C. (2018). Summary of Progress In The Development Of A Time-to-contact Autorotation Cueing System. In International Powered Lift Conference 2018. We The Curious, Bristol.
Jump, M., Alam, M., Rogers, J., & Eberle, B. (2018). Progress in the Development of a Time-To-Contact Autorotation Cueing System. In 44th European Rotorcraft Forum (pp. 1-12). Delft, Netherlands.
Aerodynamic modeling of the Skywalker X8 Fixed-Wing Unmanned Aerial Vehicle (Conference Paper)
Gryte, K., Hann, R., Alam, M., Rohac, J., Johansen, T. A., & Fossen, T. I. (2018). Aerodynamic modeling of the Skywalker X8 Fixed-Wing Unmanned Aerial Vehicle. In 2018 International Conference on Unmanned Aircraft Systems. Dallas, TX, USA: IEEE Xplore. doi:10.1109/ICUAS.2018.8453370DOI: 10.1109/ICUAS.2018.8453370
Progress in the development of a time-to-contact autorotation cueing system (Conference Paper)
Jump, M., Alam, M., Rogers, J., & Eberle, B. (2018). Progress in the development of a time-to-contact autorotation cueing system. In 44th European Rotorcraft Forum 2018, ERF 2018 Vol. 2 (pp. 777-788).
2017
On the internal stability of non‐linear dynamic inversion: application to flight control (Journal article)
Alam, M., & Celikovsky, S. (2017). On the internal stability of non‐linear dynamic inversion: application to flight control. IET Control Theory & Applications, 11(12), 1849-1861. doi:10.1049/iet-cta.2016.1067DOI: 10.1049/iet-cta.2016.1067
Validation of nonlinear integrated navigation solutions (Journal article)
Rohac, J., Hansen, J. M., Alam, M., Sipos, M., Johansen, T. A., & Fossen, T. I. (2017). Validation of nonlinear integrated navigation solutions. Annual Reviews in Control, 43. doi:10.1016/j.arcontrol.2017.03.006DOI: 10.1016/j.arcontrol.2017.03.006
2016
Robust Hover Mode Control of a Tiltrotor Using Nonlinear Control Technique (Conference Paper)
Alam, M., Celikovsky, S., & Walker, D. (2016). Robust Hover Mode Control of a Tiltrotor Using Nonlinear Control Technique. In AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2016-0359DOI: 10.2514/6.2016-0359
Robust hover mode control of a tiltrotor using nonlinear control technique (Conference Paper)
Alam, M., Celikovsky, S., & Walker, D. (2016). Robust hover mode control of a tiltrotor using nonlinear control technique. In 2016 AIAA Guidance, Navigation, and Control Conference.
2015
Calibration of a multi-sensor inertial measurement unit with modified sensor frame (Conference Paper)
Alam, M., Sipos, M., Rohac, J., & Simanek, J. (2015). Calibration of a multi-sensor inertial measurement unit with modified sensor frame. In 2015 IEEE International Conference on Industrial Technology (ICIT). IEEE. doi:10.1109/icit.2015.7125387DOI: 10.1109/icit.2015.7125387
Alam, M., & Rohac, J. (2015). Adaptive data filtering of inertial sensors with variable bandwidth.. Sensors (Basel, Switzerland), 15(2), 3282-3298. doi:10.3390/s150203282DOI: 10.3390/s150203282
Active gust load alleviation system for flexible aircraft: Mixed feedforward/feedback approach (Journal article)
Alam, M., Hromcik, M., & Hanis, T. (2015). Active gust load alleviation system for flexible aircraft: Mixed feedforward/feedback approach. Aerospace Science and Technology, 41, 122-133. doi:10.1016/j.ast.2014.12.020DOI: 10.1016/j.ast.2014.12.020
2014
Combined Feedforward/feedback Gust Load Alleviation Control for Highly Flexible Aircraft (Conference Paper)
Alam, M. (2014). Combined Feedforward/feedback Gust Load Alleviation Control for Highly Flexible Aircraft. In Proceedings of 2014 PEGASUS-AIAA Student Conference Vol. 1 (pp. 1-10). Prague. Retrieved from http://measure.feld.cvut.cz/groups/lis/StudentConference.php
