Abstract:In this paper, a robust control method based on the uncertainty and disturbance estimator (UDE) is developed to achieve the attitude tracking control for a quadrotor. To facilitate the control design, the coupled terms in the roll, pitch and yaw dynamics are lumped into the uncertainty term and the remained dynamics can be regarded as decoupled subsystems. As a result, for each subsystem, the lumped uncertainty term contains all the coupled terms, uncertainties and disturbances, then the UDE method is applied … Show more
“…The UDE-based control method was proposed in [27], whose basic idea is that, in the frequency domain, an engineering signal can be approximated by putting it through a filter with the appropriate bandwidth. In recent years, the remarkable performance of the UDE strategy has been validated through various applications, such as servomotor [28,29], variable-speed wind turbine [30], power system [31,32], and UAV [33][34][35].…”
This paper presents an autonomous landing control approach for a quadrotor unmanned aerial vehicle subject to wind disturbance and three-dimensional movements of the landing platform. To achieve an accurate relative position estimation of the quadrotor to the landing platform, a camera, a distance sensor, and a single-board computer are integrated to the quadrotor. The coordinate transformation is introduced to deal with the constraint that only the relative position information is available. The impacts of unknown ship motions are treated as part of the lumped uncertainty terms. Then, the uncertainty and disturbance estimator-based controllers are developed to achieve the accurate relative position control of the quadrotor while dealing with unknown ship motions, ground effect, state couplings, and external disturbances. The uncertainty and disturbance estimator filter is designed based on the internal model principle to enhance the performance of the developed controller. The reference model of the relative altitude controller is modified to ensure the accurate tracking of descending commands. To maximize the capability of the developed controller, a parameter selection guideline based on the derived ship heave acceleration spectrum is provided. Both numerical simulations and flight experiments are carried out to demonstrate the effectiveness of the developed approach.
“…The UDE-based control method was proposed in [27], whose basic idea is that, in the frequency domain, an engineering signal can be approximated by putting it through a filter with the appropriate bandwidth. In recent years, the remarkable performance of the UDE strategy has been validated through various applications, such as servomotor [28,29], variable-speed wind turbine [30], power system [31,32], and UAV [33][34][35].…”
This paper presents an autonomous landing control approach for a quadrotor unmanned aerial vehicle subject to wind disturbance and three-dimensional movements of the landing platform. To achieve an accurate relative position estimation of the quadrotor to the landing platform, a camera, a distance sensor, and a single-board computer are integrated to the quadrotor. The coordinate transformation is introduced to deal with the constraint that only the relative position information is available. The impacts of unknown ship motions are treated as part of the lumped uncertainty terms. Then, the uncertainty and disturbance estimator-based controllers are developed to achieve the accurate relative position control of the quadrotor while dealing with unknown ship motions, ground effect, state couplings, and external disturbances. The uncertainty and disturbance estimator filter is designed based on the internal model principle to enhance the performance of the developed controller. The reference model of the relative altitude controller is modified to ensure the accurate tracking of descending commands. To maximize the capability of the developed controller, a parameter selection guideline based on the derived ship heave acceleration spectrum is provided. Both numerical simulations and flight experiments are carried out to demonstrate the effectiveness of the developed approach.
“…demonstrated through real flight experiment studies. Compared with previous UDE works on quadrotor attitude and height control [25,28], this paper mainly focuses on the horizontal position controller development.…”
Section: The Effectiveness Of the Developed Control Strategy Ismentioning
confidence: 99%
“…From the block diagram of the overall control system (Fig. 2), it could be seen that the cascaded inner-outer loop control structure is utilized to deal with the underactuation, where the inner loop is the attitude controller and the outer loop is the position [25], this paper will focus on the controller development for the position subsystems. From the x, y dynamics (1) and (2), it could be seen that the control inputs for horizontal motions are in nonaffine forms, which leads to the failure of using feedback linearization.…”
Section: Control Design Ude-based Position Controller Developmentmentioning
confidence: 99%
“…The basic idea of the UDE method is that in the frequency domain an engineering signal (the model uncertainty and external disturbance) can be approximated by putting it through a filter with the appropriate bandwidth. The remarkable performance of the UDE strategy has been demonstrated in recent years through both theories [22,23,24] and practical applications [25,26,27,28].…”
In this paper, the uncertainty and disturbance estimator (UDE)-based position controllers are developed to achieve the robust position control of a quadrotor using only onboard sensing. Firstly, in order to accurately estimate the positions of the quadrotor in GPS-denied environments, an open source high speed optical flow sensor PX4FLOW is adopted. Secondly, the UDE-based controllers are developed to handle the challenges brought by the highly nonlinear quadrotor position dynamics, including underactuation, coupling, nonaffine inputs, model uncertainties and external disturbances. Real flight experiments, including hover and disturbance rejection are carried out to demonstrate the effectiveness of the developed UDE-based controllers.
This paper addresses the problem of autonomous trajectory tracking control for a quadrotor in a global positioning system (GPS)-denied environment using only onboard sensing. To achieve that goal, it requires accurate estimation of quadrotor states followed by proper control actions. For the position estimation in a GPS-denied environment, an open source high speed optical flow sensor PX4FLOW is adopted. As for the quadrotor control, there are several challenges due to its highly nonlinear system dynamics, such as underactuation, coupling, model uncertainties, and external disturbances. To deal with those challenges, the cascaded inner–outer uncertainty and disturbance estimator (UDE)-based robust control scheme has been developed and applied to the attitude and position control of a quadrotor. Extensive real flight experiments, including attitude stabilization, hover, disturbance rejection, trajectory tracking, and comparison with the proportional–integral–derivative (PID) controller are carried out to demonstrate the effectiveness of the developed UDE-based controllers.
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