Nonlinear modeling and designing transition flight control scenarios for a dual thrust hybrid UAV
N Mohammadi, M Tayefi, M Zhu - International Journal of Intelligent …, 2024 - Springer
Researchers have recently focused on studying the flight dynamics and control of
multicopters and fixed-wing aerial vehicles. However, investigating the transition phase …
multicopters and fixed-wing aerial vehicles. However, investigating the transition phase …
Model-Based Optimization Approach for PID Control of Pitch–Roll UAV Orientation
This study focuses on the modeling and control optimization of the pitch–roll angles
orientation in a quad-rotor UAV (unmanned aerial vehicle) drone system. To address the …
orientation in a quad-rotor UAV (unmanned aerial vehicle) drone system. To address the …
Consensus-Based Powered Cruise and Yaw Controls for Unmanned Aerial Vehicle with Distributed Electric Propulsion System
The distributed electric propulsion (DEP) system has been favored over the conventional
centralized propulsion system in applications of unmanned aerial vehicles (UAV). However …
centralized propulsion system in applications of unmanned aerial vehicles (UAV). However …
[PDF][PDF] Integrating second order sliding mode control and anomaly detection using auto-encoder for enhanced safety and reliability of quadrotor UAVs
This paper presents a comprehensive framework for enhancing the safety and reliability of
quadrotor UAVs by integrating secondorder sliding mode control (2-SMC) and an advanced …
quadrotor UAVs by integrating secondorder sliding mode control (2-SMC) and an advanced …
Vertical take-off and hover to cruise transition for a hybrid UAV using model predictive controller and MPC allocation
N Mohammadi, M Tayefi, M Zhu - Aircraft Engineering and Aerospace …, 2023 - emerald.com
Purpose Dual-thrust hybrid unmanned aerial vehicle (UAV) technology offers a highly robust
and efficient system that incorporates the take-off and landing capabilities of rotary-wing …
and efficient system that incorporates the take-off and landing capabilities of rotary-wing …