Design, Modeling, and Control of a Fully Actuated Multirotor with Multidirectional Thrusts
This paper introduces a novel multirotor Unmanned Aerial Vehicles (UAV) configuration with inclinable rotors, extendable arms, and a spatial arrangement, categorized under a new classification system based on articulation and rotor dispersion. A comprehensive nonlinear mathematical model is developed to account for asymmetry, rotor placement, and dynamic behavior. The model is validated through MATLAB simulations across multiple scenarios, demonstrating precise complex trajectory tracking. The proposed PID control parameters were optimized using Particle Swarm Optimization (PSO), achieving significant improvements in control effort and energy efficiency. Results highlight the UAV’s adaptability and performance, providing a foundation for future research on robust control methods to handle real-world disturbances.
Authors
- Saddam Hocine Derrouaoui (ORCID: https://orcid.org/0000-0001-5441-8224)
- Yasser Bouzid (ORCID: https://orcid.org/0000-0002-8400-9912)
- Mariyam Jameelah Ghazali
- Mahmoud Belhocine (ORCID: https://orcid.org/0000-0003-3495-7444)
Institutions
- Polytechnic School of Algiers (DZ)
- Centre de Développement des Technologies Avancées (DZ)
Publication Details
- Journal
- Unmanned Systems
- Published
- 2025-04-24
- DOI
- https://doi.org/10.1142/s2301385026500391
- Primary Topic
- Aerospace Engineering and Control Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.00