Passivity-based simple adaptive control for quadrotor helicopter in the presence of actuator dynamics

Mokhtari, Khalil; Aribi, Mourad

doi:10.1109/icmic.2016.7804222

Cited by 1 publication

(2 citation statements)

References 21 publications

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“…it can be verified that the second inequality in ( 34) is a necessary condition for (42). Combining ( 22), (34), and (42) yields the following comprehensive conditions to guarantee that…”

Section: Stepmentioning

confidence: 99%

“…This is because the relationship between the controller parameters and the system bandwidth needs to adhere to the limitations imposed by the dynamics of the actuator to guarantee system stability, as demonstrated in the author's previous work [30]. In most cases, actuator dynamics are approximated by a first-order model [31][32][33][34]. Nevertheless, in the studies conducted by Qi et al [35] and Qin et al [24], the actuators are described as first-order plus time-delay (FOPTD) models by using thrust test platforms to precisely identify the model parameters, which are more consistent with the actual quadrotor drone actuator characteristics.…”

Section: Introductionmentioning

confidence: 99%

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UDE-Based Dynamic Surface Control for Quadrotor Drone Attitude Tracking under Non-Ideal Actuators

Qin

Tang

et al. 2023

Drones

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Quadrotor drone attitude tracking is inevitably affected by the combination of model uncertainties, external disturbances, and non-ideal actuator dynamics during stable flight and complex maneuvers. In order to achieve precise attitude control in these situations, a cascade-structured dynamic surface control (DSC) strategy is proposed based on an uncertainty and disturbance estimator (UDE), considering the actuator dynamics as represented by a first-order plus time-delay model. The DSC scheme is used to transform the original attitude dynamics system into a set of interconnected subsystems. On the one hand, the mismatched disturbances in the attitude kinematics and dynamics loops are converted into matched disturbances to accommodate the structural constraints of the UDE so that these disturbances, as well as the non-ideality caused by the actuator time delay, are estimated and compensated for by the approach. On the other hand, the “complexity explosion” problem is addressed by the first-order filter employed by DSC. The ultimate boundedness of the closed-loop system is proven while the parameter design constraints are provided. MATLAB Simulink simulations are conducted to demonstrate the desirability of considering actuator dynamics and to verify that the proposed control strategy can relax the constraints of the control parameters and enable a higher accuracy.

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“…it can be verified that the second inequality in ( 34) is a necessary condition for (42). Combining ( 22), (34), and (42) yields the following comprehensive conditions to guarantee that…”

Section: Stepmentioning

confidence: 99%