Sliding mode control of directly excited structural dynamic model of twin-tailed fighter aircraft

Mahgoub, Youssef; El-Badawy, Ayman

doi:10.1016/j.jfranklin.2021.10.017

Cited by 3 publications

(2 citation statements)

References 21 publications

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“…In addition to OLFC and SDREC, SMC was proposed by Utkin in 1992 22 , and it is widely used to control vibration together with other SMC-based strategies. In 2009, the SMC was applied to chaos control of systems with nonlinearities plus parametric uncertainties 23 ; in 2018, Amin et al 24 proposed a robust SMC to eliminate chattering in a one-dimensional nonlinear system of the functionally graded and homogeneous nanobeams; in 2021, Youssef and Ayman utilized 25 an integral SMC to suppress the twin-tails buffeting of a fighter aircraft. In 2006, conventional SMC was combined with fuzzy rules to alleviate the impacts of uncertainty in dynamic systems, and an innovative control method, fuzzy sliding mode control (FSMC), was proposed for Duffing system synchronization 26 .…”

Section: Control Of Large Amplitude Limit Cycle Of a Multi-dimensiona...mentioning

confidence: 99%

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Control of large amplitude limit cycle of a multi-dimensional nonlinear dynamic system of a composite cantilever beam

Sun,

Li,

Liu

2024

Sci Rep

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For the first time, a control strategy based on Fuzzy Sliding Mode Control is implemented in the control of a large amplitude limit cycle of a composite cantilever beam in a multi-dimensional nonlinear form. In the dynamic model establishment of the investigated structure, the higher-order shearing effect is applied, as well as the second-order discretization. Numerical simulation demonstrates that a multi-dimensional nonlinear dynamic system of the investigated structure is demanded for accurate estimation of large amplitude limit cycle responses. Therefore, a control strategy is employed to effectively suppress such responses of the beam in multi-dimensional nonlinear form.

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Section: Control Of Large Amplitude Limit Cycle Of a Multi-dimensiona...mentioning

confidence: 99%

“…With the control strategy in Eqs. (21)(22)(23)(24)(25)(26), the active vibration control of the large amplitude limit cycle discovered based on the governing equation in Eq. ( 10) is ready.…”

Section: Control Strategymentioning

confidence: 99%

Control of large amplitude limit cycle of a multi-dimensional nonlinear dynamic system of a composite cantilever beam

Sun,

Li,

Liu

2024

Sci Rep

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Wind turbulence modeling for real-time simulation

Hajjem

Victor

Melchior

et al. 2023

Fract Calc Appl Anal

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Control of a Flapping Wing Aerial Vehicle in the Presence of Matched and Mismatched Disturbances

2022

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The work presented in this paper addresses trajectory tracking and position control of a six-degrees-of-freedom flapping wing micro aerial vehicle (FWMAV) in the presence of matched and mismatched disturbances. FWMAV is an unstable system which is affected by various disturbances. These disturbances can be classified into matched and mismatched disturbances according to their entrance via the same or different channels from control inputs. In order to handle these disturbances, an integral command-filtered block backstepping controller is applied to a nonlinear high-fidelity time-variant dynamic model. The stability of the proposed controller and the ultimate boundedness of the tracking error is derived based on Lyapunov stability arguments. Finally, the control law is validated by various simulation studies on the high-fidelity model. The proposed controller performance proves its ability to successfully track the arbitrary desired reference trajectories with feasible control effort in the presence of both constant and time-varying matched and mismatched disturbances.

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Sliding mode control of directly excited structural dynamic model of twin-tailed fighter aircraft

Cited by 3 publications

References 21 publications

Control of large amplitude limit cycle of a multi-dimensional nonlinear dynamic system of a composite cantilever beam

Control of large amplitude limit cycle of a multi-dimensional nonlinear dynamic system of a composite cantilever beam

Wind turbulence modeling for real-time simulation

Control of a Flapping Wing Aerial Vehicle in the Presence of Matched and Mismatched Disturbances

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