Coupling effect-triggered control strategy for hypersonic flight vehicles with finite-time convergence

DOI10.1007/S11071-018-4611-5zbMath1439.70035OpenAlexW2896960868WikidataQ129054121 ScholiaQ129054121MaRDI QIDQ784036

D. Kharzeev

Publication date: 5 August 2020

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-018-4611-5

zbMATH Keywords

sliding modeattitude controlcoupling effecthypersonic flight vehicles

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Finite-time stability (93D40)

Related Items (2)

High-order sliding mode observer-based trajectory tracking control for a quadrotor UAV with uncertain dynamics ⋮ Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach

Cites Work

• Quantification of interaction in multiloop control systems using directed spectral decomposition
• Static anti-windup design for nonlinear Markovian jump systems with multiple disturbances
• An integral predictive/nonlinear \(\mathcal H_{\infty}\) control structure for a quadrotor helicopter
• Guaranteeing prescribed output tracking performance for air-breathing hypersonic vehicles via non-affine back-stepping control design
• Barrier Lyapunov function-based adaptive control for hypersonic flight vehicles
• Event-triggered robust adaptive control for uncertain nonlinear systems preceded by actuator dead-zone
• An adaptive sliding mode differentiator for actuator oscillatory failure case reconstruction
• Self-scheduled robust decoupling control with \(H_\infty\) performance of hypersonic vehicles
• Composite anti-disturbance control for Markovian jump nonlinear systems via disturbance observer
• MIMO interaction measure and controller structure selection
• Compensator based output feedback sliding mode controller design
• Event-Triggered Real-Time Scheduling of Stabilizing Control Tasks
• Time-domain performance limitations arising from decentralized architectures and their relationship to the RGA
• A review of methods for input/output selection

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