Dynamic System Emulation: Fixed Wing Dynamics on a Multicopter
Organizations: Department of Electrical and Computer Engineering, Aarhus University, Denmark
Abstract
This work presents a control framework that enables a multicopter equipped with a two-axis gimbal to emulate the flight dynamics of a fixed-wing aircraft. The goal is to provide an operationally simple platform for training and simulation that avoids the aerodynamic constraints of fixed-wing vehicles, such as minimum airspeed and nonholonomic constraints. A state-input mapping between the two platforms is derived using dynamic feedback linearization. The framework is evaluated on representative fixed-wing manoeuvres. Results show high-fidelity emulation under nominal conditions. While evaluations are conducted in simulation, the approach establishes a practical path toward hardware deployment for pilot training, autonomy research, and controller benchmarking.
Figures & tables
| Fixed-Wing (Redbull Edge 540) | |
| Mass | 530 kg |
| Moments of inertia | (2419, 2133, 4552) kg·m² |
| Wingspan | 7.40 m |
| Wing Area | 9.10 m² |
| Mean Chord | 1.23 m |
| Max Speed | 118 m/s |
Aerial Robotics
Aerial robotics studies the design, perception, control, and coordination of flying robots for navigation, inspection, transport, and physical interaction.
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