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Mushfiqul Alam
Mushfiqul Alam
Lecturer in Flight Dynamics and Control
Verified email at cranfield.ac.uk - Homepage
Title
Cited by
Cited by
Year
Aerodynamic modeling of the skywalker x8 fixed-wing unmanned aerial vehicle
K Gryte, R Hann, M Alam, J Roháč, TA Johansen, TI Fossen
2018 International Conference on Unmanned Aircraft Systems (ICUAS), 826-835, 2018
712018
Adaptive data filtering of inertial sensors with variable bandwidth
M Alam, J Rohac
Sensors 15 (2), 3282-3298, 2014
372014
Active gust load alleviation system for flexible aircraft: Mixed feedforward/feedback approach
M Alam, M Hromcik, T Hanis
Aerospace Science and Technology 41, 122-133, 2015
362015
On the internal stability of non‐linear dynamic inversion: application to flight control
M Alam, S Celikovsky
IET Control Theory & Applications 11 (12), 1849-1861, 2017
122017
Validation of nonlinear integrated navigation solutions
J Rohac, JM Hansen, M Alam, M Sipos, TA Johansen, TI Fossen
Annual reviews in control 43, 91-106, 2017
112017
Robust hover mode control of a tiltrotor using nonlinear control technique
M Alam, S Celikovsky, D Walker
AIAA Guidance, Navigation, and Control Conference, 0359, 2016
92016
INS/GNSS Localization Using 15 State Extended Kalman Filter
M Alam, G Moreno, M Sipos, J Rohac
International Conference in Aerospace for Young Scientists 1 (1), 425-435, 2016
82016
Calibration of a multi-sensor inertial measurement unit with modified sensor frame
M Alam, M Sipos, J Rohac, J Simanek
2015 IEEE International Conference on Industrial Technology (ICIT), 1984-1989, 2015
72015
Structural load alleviation using distributed delay shaper: Application to flexible aircraft
M Alam, M Hromcik
Control Engineering Practice 89, 130-142, 2019
42019
Progress in the Development of a Time-To-Contact Autorotation Cueing System
M Jump, M Alam, J Rogers, B Eberle
44th European Rotorcraft Forum, 1-12, 2018
42018
Development of Inertial Navigation System Using Tactical Grade Sensors
M BÍLÝ, M ALAM
Proceedings of the 19th International Scientific Student Conferenece POSTER, 2015
42015
Can Time-To-Contact Be Used To Model A Helicopter Autorotation?
M Alam, N Jump, Michael, Cameron
8th Asian/Australian Rotorcraft Forum 1 (1), 1-8, 2019
32019
Dynamic inversion-based flare control law for autonomous helicopter autorotation
U Saetti, JD Rogers, M Alam, M Jump, N Cameron
AIAA SCITECH 2022 Forum, 1645, 2022
22022
Oblique Wing: Future Generation Transonic Aircraft
M Alam, K Narenathreyas
International Journal of Mechanical, Aerospace, Industrial and Mechatronics …, 2014
22014
Combined Feedforward/feedback Gust Load Alleviation Control for Highly Flexible Aircraft
M Alam
Proceedings of 2014 PEGASUS-AIAA Student Conference, 1-10, 2014
22014
Tau theory-based flare control in autonomous helicopter autorotation
U Saetti, J Rogers, M Alam, M Jump
Aerospace 11 (1), 33, 2023
12023
Development of High-Fidelity Saab 340B Aerodynamic Model
M Millidere, M Alam, S Place, J Whidborne
AIAA SCITECH 2023 Forum, 0909, 2023
12023
Rapid Method for Computing Reachable Landing Distances in Helicopter Autorotative Descent
BF Eberle, JD Rogers, M Alam, M Jump
Journal of Aerospace Information Systems 19 (7), 504-510, 2022
12022
Gust Load Alleviation System for BWB (Blended Wing Body) Flexible Aircraft
M Alam
12013
SAAB 340B Aerodynamic Model Development Using Binary Particle Swarm Optimization
M Millidere, M Alam, S Place, J Whidborne
AIAA SCITECH 2024 Forum, 1495, 2024
2024
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