The role of propeller aerodynamics in the model of a quadrotor UAV
By P. Bristeau, Philippe Martin, Erwan Salaün, Nicolas Petit. 2009
195 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computer Networks and Communications, Control and Systems Engineering
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
- Moses Bangura
- Davide Scaramuzza
- Raffaello D'Andrea
- Matthias Faessler
- Markus Achtelik
- Angela P. Schoellig
- Antonio Franchi
- Nicolas Petit
In Computer Networks and Communications
In Control and Systems Engineering
- Moses Bangura
- Davide Scaramuzza
- Raffaello D'Andrea
- Matthias Faessler
- Angela P. Schoellig
- Antonio Franchi
- Sergei Lupashin
- Nicolas Petit
Citations in the corpus
- Differential Flatness of Quadrotor Dynamics Subject to Rotor Drag for Accurate Tracking of High-Speed Trajectories (2017, background): “Rotor drag effects influencing a quadrotor’s dynamics were investigated in [4] and [5] where also a control law was presented, which considers these dynamics.”
- A simple learning strategy for high-speed quadrocopter multi-flips (2010, background): “For example, while much research recently has been focused on extremely precise modeling of propeller effects in quadro-copters [10], the identification of all parameters requires devoted, carefully-designed experiments with an extremely cautious treatment of measurement errors, unwanted aerodynamic…”
- The true role of accelerometer feedback in quadrotor control (2010, background): “…Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA, USA erwan.salaun@gatech.edu velocities; [14] physically motivates the presence of effects nearly linear w.r.t the quadrotor linear and angular velocities, but provides no experimental data and is concerned only with the…”
- Aerodynamics and Control of Quadrotors (2017, methodology): “In addition to PID, proportional derivative (PD) and linear quadratic (LQ) control have also been used for attitude stabilisation using Euler angle representation of the attitude of the vehicle (Castillo et al. [2004a]; Salazar-Cruz et al. [2005]; Erginer and Altuğ [2007]; Bouabdallah et al.”
- The Navigation and Control technology inside the AR.Drone micro UAV (2011, methodology): “Drone contains state-of-the art low-cost navigation methods, video processing algorithms, combined with an innovative usage of an aerodynamics model which previous fine theoretical studies (see Bristeau et al. [2009]) permit to stress crucial information serving as a robust estimate of the air speed”
- Nonlinear feedback control of Quadrotors exploiting First-Order Drag Effects (2017, unknown): “In Bristeau et al. (2009), Pounds et al. (2010), Bangura and Mahony (2012), Mahony et al. (2012) and Bangura et al. (2016), it has been considered that due to the natural flexibility of the blades, small-scale hingeless rotors exhibit similar mechanical behavior to the one produced by hinged rotors…”