2013
DOI: 10.1109/access.2013.2260794
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Robust Optimal Control of Quadrotor UAVs

Abstract: This paper provides the design and implementation of an L 1 -optimal control of a quadrotor unmanned aerial vehicle (UAV). The quadrotor UAV is an underactuated rigid body with four propellers that generate forces along the rotor axes. These four forces are used to achieve asymptotic tracking of four outputs, namely the position of the center of mass of the UAV and the heading. With perfect knowledge of plant parameters and no measurement noise, the magnitudes of the errors are shown to exponentially converge … Show more

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Cited by 88 publications
(41 citation statements)
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“…Though there are proposals for advanced adaptive control using artificial neural networks [30], or optimal robust control [31], in this section we will approach the problem from the point of view of classical Proportional Integral Derivative (PID) controllers [24]. For this section, we follow the modeling approach of quadrotor dynamics and kinematics proposed in [32] consisting of a collection of equations, involving spatial coordinates, local angles, torques, angular speed of rotors, and the electric modeling.…”
Section: Quadrotor Control Systemmentioning
confidence: 99%
“…Though there are proposals for advanced adaptive control using artificial neural networks [30], or optimal robust control [31], in this section we will approach the problem from the point of view of classical Proportional Integral Derivative (PID) controllers [24]. For this section, we follow the modeling approach of quadrotor dynamics and kinematics proposed in [32] consisting of a collection of equations, involving spatial coordinates, local angles, torques, angular speed of rotors, and the electric modeling.…”
Section: Quadrotor Control Systemmentioning
confidence: 99%
“…In recent years, the research on quadrotor vehicles has attracted great interest due to the wide range of civil and military applications, and many achievements have been made [1,2]. As a new kind of unmanned aerial vehicle (UAV), the quadrotor is a small rotorcraft with four propellers driven by four direct current (DC) motors respectively [3].…”
Section: Introductionmentioning
confidence: 99%
“…For a fuzzy model having q input parameters, for each input parameters p MFs are defined. Then, for a full fuzzy inference system q p fuzzy rules are required, such as in [11,12] a fuzzy inference system has been designed where there are 12 input variables and for each variable five MFs are allocated. Hence, the entire number of rules obligatory to completely implement the system are 5 12 .…”
mentioning
confidence: 99%