Robust Missile Autopilots With Finite-Time Convergence

DOI10.1002/ASJC.1183zbMath1348.93095OpenAlexW1498339571MaRDI QIDQ2828542

Shaoming He, Jiang Wang, Defu Lin

Publication date: 26 October 2016

Published in: Asian Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/asjc.1183

zbMATH Keywords

finite-time convergencenonlinear disturbance observerexternal disturbancemissile autopilotaerodynamic uncertaintyangle-of-attack tracking

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Nonlinear systems in control theory (93C10) Perturbations in control/observation systems (93C73) Observability (93B07) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (1)

Robust finite-time tracking for a square fully actuated class of nonlinear systems

Cites Work

• Smooth second-order sliding modes: missile guidance application
• Gain-ScheduledH_∞Control for Tensor Product Type Polytopic Plants
• Finite-time stability of cascaded time-varying systems
• Nonlinear predictive controllers for continuous systems
• Continuous finite-time stabilization of the translational and rotational double integrators
• Higher-order sliding modes, differentiation and output-feedback control
• A continuous feedback approach to global strong stabilization of nonlinear systems
• Missile autopilot design via a modified LPV synthesis technique
• Finite-Time Stability of Continuous Autonomous Systems

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