منابع مشابه
Robust Control of a Quadrotor
In this paper, a robust tracking control method for automatic take-off and trajectory tracking of a quadrotor helicopter is presented. The designed controller includes two parts: a position controller and an attitude controller. The attitude controller is designed by using the sliding mode control (SMC) method to track the desired pitch and roll angles, which are the output of position controll...
متن کاملRandomized Approaches for Control of QuadRotor UAVs
A systematic mixed deterministic-randomized approach for filter design is presented. This method has two advantages: (i) it is a computational efficient algorithm for the deterministic parameters and (ii) we can design fixed order controllers because we follow a randomization approach. Different filter forms are selected to prove the effectiveness of this algorithm and the obtained results are ...
متن کاملNonlinear Landing Control for Quadrotor UAVs
Quadrotor UAVs are one of the most preferred type of small unmanned aerial vehicles because of the very simple mechanical construction and propulsion principle. However, the nonlinear dynamic behavior requires a more advanced stabilizing control and guidance of these vehicles. In addition, the small payload reduces the amount of batteries that can be carried and thus also limits the operating r...
متن کاملrobust control of a quadrotor
in this paper, a robust tracking control method for automatic take-off and trajectory tracking of a quadrotor helicopter is presented. the designed controller includes two parts: a position controller and an attitude controller. the attitude controller is designed by using the sliding mode control (smc) method to track the desired pitch and roll angles, which are the output of position controll...
متن کاملPassivity-based adaptive backstepping control of quadrotor-type UAVs
We propose a novel unified passivity-based adaptive backstepping control framework for ‘‘mixed’’ quadrotor-type unmanned aerial vehicles (UAVs), which consists of the translation dynamics with thrust force input λ ∈ R and the attitude kinematics with the angular velocity input w ∈ R3 evolving on SE(3). We also show how our proposed unified framework can be used for velocity field following, tim...
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ژورنال
عنوان ژورنال: IEEE Access
سال: 2013
ISSN: 2169-3536
DOI: 10.1109/access.2013.2260794