PID vs LQ control techniques applied to an indoor micro quadrotor
By Samir Bouabdallah, A. Noth, Roland Yves Siegwart. IEEE/RJS International Conference on Intelligent RObots and Systems, 2004
1,418 citations recorded by the source corpus.
Subfields: Computer Networks and Communications, Control and Systems Engineering
View Paper: https://www.semanticscholar.org/paper/9b510764debf0be1dbc5e068728a260f14b8fd69
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In Computer Networks and Communications
- Frank L. Lewis
- Moses Bangura
- Kamesh Subbarao
- Robert E. Mahony
- Peter Corke
- Davide Scaramuzza
- Abhijit Das
- P. Pounds
In Control and Systems Engineering
- Moses Bangura
- Davide Scaramuzza
- Robert E. Mahony
- Frank L. Lewis
- Abhijit Das
- Kamesh Subbarao
- Erwan Salaün
- Philippe Martin
Citations in the corpus
- Modelling and control of a quad-rotor robot (2006, methodology): “A variety of control techniques have been implemented successfully on quad-rotor UAVS – these include PID and LQ [Bouabdallah et al, 2004] and PD(2) [Tayebi and McGilvray, 2004] control.”
- Mathematical modeling and vertical flight control of a tilt-wing UAV (2012, neutral): “Key Words: Tilt-wing, quadrotor, PID, VTOL, hover”
- Backstepping Approach for Controlling a Quadrotor Using Lagrange Form Dynamics (2009, methodology): “References [4, 12] compared the performance of a proportional-integral-derivative (PID) controller with a LQ control law on a micro vertical take-off and landing (VTOL) test bench.”
- The true role of accelerometer feedback in quadrotor control (2010, methodology): “Accordingly, the pitch and roll angles are estimated from gyroscope and accelorometer measurements thanks to some sensor fusion algorithm: Extended Kalman Filter (EKF) [ 2 ]; complementary filter, linear [3], [7] or nonlinear [10] (see [15], [16], [17] for an account of such nonlinear filters and re”
- Aerodynamics and Control of Quadrotors (2017, methodology): “[2005]; Erginer and Altuğ [2007]; Bouabdallah et al. [2004]; Mokhtari et al. [2004] and many more). This representation does not account for the coupling that exists between the Euler angles which surfer from singularities and gimbal lock. To overcome this, Tayebi Tayebi and McGilvray [2006] propose”
- Thrust Mixing, Saturation, and Body-Rate Control for Accurate Aggressive Quadrotor Flight (2017, methodology): “Besides such cascaded loops of proportional controllers, LQR [7] and nonlinear model predictive control techniques on SO(3) [8] were successfully applied to control the full attitude of quadrotors.”