System identification of an unmanned quadcopter system using MRAN neural MF Pairan, SS Shamsudin IOP conference series: materials science and engineering 270 (1), 012019, 2017 | 20 | 2017 |
Neural network based system identification for quadcopter dynamic modelling: A review MF Pairan, SS Shamsudin, MF Zulkafli Journal of Advanced Mechanical Engineering Applications 1 (2), 20-33, 2020 | 14 | 2020 |
Dynamic modelling and control for quadcopter uav with labview and x-plane flight simulator YAA Zabidin, MF Pairan, SS Shamsudin Journal of Complex Flow 2 (2), 19-26, 2020 | 10 | 2020 |
The design of an automatic flight control system and dynamic simulation for fixed-wing unmanned aerial vehicle (UAV) using X-Plane and LabVIEW NEA Mazlan, SS Shamsudin, MF Pairan, MF Yaakub, MF Ramli Progress in Aerospace and Aviation Technology 1 (1), 56-69, 2021 | 3 | 2021 |
Autotuning PID Controllers for Quadplane Hybrid UAV using Differential Evolution Algorithm MF Pairan, S Shamsudin, MF Yaakub Journal of Aeronautics, Astronautics and Aviation 56 (1s), 341-356, 2024 | 2 | 2024 |
Real-time system identification of an unmanned quadcopter system using fully tuned radial basis function neural networks MF Pairan, SS Shamsudin, MF Yaakub, MSM Anwar International Journal of Modelling, Identification and Control 37 (2), 128-139, 2021 | 2 | 2021 |
A comparative study on longitudinal dynamics stability between two aircraft models MF Pairan, B Basuno, MD Firdaus, SS Shamsudin Progress in Aerospace and Aviation Technology 2 (2), 81-91, 2022 | 1 | 2022 |
The Structural Design and Aerodynamics Analysis for a Hybrid VTOL Fixed-Wing Drone for Parcel Delivery Applications S Chakraverty, MF Zulkafli, MF Pairan, MNMS See, IK Mahmud Progress in Aerospace and Aviation Technology 2 (1), 41-52, 2022 | | 2022 |
The Application of Ansys-Fluent Software for Aerodynamic Analysis on Rectangular and Moderate Swept Wing Planform MZM Shah, B Basuno, A Abdullah, MF Pairan Journal of Engineering and Technology (JET) 12 (1), 11-32, 2021 | | 2021 |
Assessing helicopter main rotor blade critical area using blade element theory in the cases of forward speed and blade collective pitch angle increments MF Yaakub, SJMM Saleh, A Abdullah, N Ahmad, RN Mohd, MF Pairan | | 2019 |
Real-time identification of an unmanned quadcopter flight dynamics using fully tuned radial basis function network MF Pairan Universiti Tun Hussein Onn Malaysia, 2018 | | 2018 |
Flight Control System Design for a Rotorcraft-Based Unmanned Aerial System using Pole Placement and LQR-Based PID Tuning Techniques SH Yi, SS Shamsudin, MF Pairan | | |