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Two-time-scale robust output feedback control for aircraft longitudinal dynamics via sliding mode control and high-gain observer

This paper presents output feedback control for longitudinal dynamics of fixed-wing aircraft using singular perturbation techniques. The longitudinal dynamic model is separated into two timescales. A composite feedback control law based on sliding mode control (SMC) is designed for slow and fast sub...

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Gorde:
Xehetasun bibliografikoak
Egile Nagusiak: Abid Raza, Fahad Mumtaz Malik, Naveed Mazhar, Rameez Khan
Formatua: Artigo
Hizkuntza:Inglês
Argitaratua: Elsevier 2022-06-01
Saila:Alexandria Engineering Journal
Gaiak:
Sarrera elektronikoa:http://www.sciencedirect.com/science/article/pii/S1110016821006864
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