Design, Modeling, and Control Allocation of a Heavy-Lift Aerial Vehicle Consisting of Large Fixed Rotors and Small Tiltrotors
Author:
Affiliation:
1. Microelectronics, Guidance and Electro-Optics Division, Aselsan Inc., Ankara, Turkey
2. Department of Electrical and Electronics Engineering, Middle East Technical University, Ankara, Turkey
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering
Link
http://xplorestaging.ieee.org/ielx7/3516/9924619/09721266.pdf?arnumber=9721266
Reference40 articles.
1. Design and optimal control of a tiltrotor micro-aerial vehicle for efficient omnidirectional flight
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3. Cogging torque disturbance rejection for a low-cost gimbal motor and a controller design with practical considerations;özdo?an;Proc IEEE 12th Asian Control Conf,0
4. Performance of minimum energy controllers on tiltrotor aircraft
5. Subspace Identification and ARX Modeling
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1. Research of Transition Corridor and Optimal Trajectory for Front-Tilt-Quadplane eVTOL Aircraft;2023 6th International Conference on Electronics Technology (ICET);2023-05-12
2. Robust Attitude Controller Design for an Uncommon Quadrotor With Big and Small Tilt Rotors;Journal of Mechanisms and Robotics;2023-02-21
3. A New Overactuated Multirotor: Prototype Design, Dynamics Modeling, and Control;IEEE Transactions on Industrial Electronics;2023
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