Model-free–based terminal SMC of quadrotor attitude and position
H Wang, X Ye, Y Tian, G Zheng… - IEEE Transactions on …, 2016 - ieeexplore.ieee.org
In this paper, a model-free-based terminal sliding-mode control (MFTSMC) strategy is
developed to control the attitude and position of a quadrotor whose model includes …
developed to control the attitude and position of a quadrotor whose model includes …
Dynamics modelling and linear control of quadcopter
In this paper, a cascade PID feedback control algorithm is proposed to stabilize the attitude
of a quadcopter so that the balancing state can be ensured in spite of disturbances. A …
of a quadcopter so that the balancing state can be ensured in spite of disturbances. A …
Structure regulator for the perturbations attenuation in a quadrotor
In this work, we study the structure regulator for the perturbations attenuation which is based
on the infinite structure regulator. The structure regulator is able to attenuate the …
on the infinite structure regulator. The structure regulator is able to attenuate the …
Model-free-based single-dimension fuzzy SMC design for underactuated quadrotor UAV
The underactuated quadrotor unmanned aerial vehicle (UAV) is one of the nonlinear
systems that have few actuators as compared to the degree of freedom (DOF); thus, it is a …
systems that have few actuators as compared to the degree of freedom (DOF); thus, it is a …
Nonlinear robust H-infinity PID controller for the multivariable system quadrotor
JP Ortiz, LI Minchala, MJ Reinoso - IEEE Latin America …, 2016 - ieeexplore.ieee.org
This paper presents the methodology of design of a nonlinear robust controller for attitude
regulation and its implementation in an experimental platform of an unmanned aerial vehicle …
regulation and its implementation in an experimental platform of an unmanned aerial vehicle …
MIMO PID controller tuning method for quadrotor based on LQR/LQG theory
R Guardeño, MJ López, VM Sánchez - Robotics, 2019 - mdpi.com
In this work, a new pre-tuning multivariable PID (Proportional Integral Derivative) controllers
method for quadrotors is put forward. A procedure based on LQR/LQG (Linear Quadratic …
method for quadrotors is put forward. A procedure based on LQR/LQG (Linear Quadratic …
Completion of collision avoidance control algorithm for multicopters based on geometrical constraints
HLNN Thanh, SK Hong - IEEE Access, 2018 - ieeexplore.ieee.org
The collision avoidance problem for multicopters is solved based on the combination of
geometrical constraints and kinematics equation through this paper. The method is …
geometrical constraints and kinematics equation through this paper. The method is …
Controlling a quadrotor UAV by means of a fractional nested saturation control
In this paper, a fractional nonlinear control strategy based on the nested saturations
technique and the Caputo-Fabrizio derivative for a quadrotor aircraft, to maintain desired …
technique and the Caputo-Fabrizio derivative for a quadrotor aircraft, to maintain desired …
Robust trajectory‐tracking control of a PVTOL under crosswind
C Aguilar‐Ibanez, H Sira‐Ramirez… - Asian Journal of …, 2019 - Wiley Online Library
This work proposes a robust controller to solve the trajectory‐tracking control problem of
planar vertical take‐off and landing (PVTOL) aircraft under crosswind. The controller …
planar vertical take‐off and landing (PVTOL) aircraft under crosswind. The controller …
Simple nonlinear control of quadcopter for collision avoidance based on geometric approach in static environment
A simple, robust nonlinear controller for quadcopters to avoid collisions, based on the
geometry approach and kinematics equation, is proposed. The controller allows the …
geometry approach and kinematics equation, is proposed. The controller allows the …