Takeoff/landing control based on acceleration measurements for VTOL aircraft

DOI10.1016/J.JFRANKLIN.2013.06.020zbMath1293.93728OpenAlexW2092079136MaRDI QIDQ398275

Xinhua Wang

Publication date: 15 August 2014

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2013.06.020

zbMATH Keywords

estimationstabilizationfinite-time stabilitynonlinear double integratorvertical takeoff and landing (VTOL) aircraft

Mathematics Subject Classification ID

Application models in control theory (93C95) Estimation and detection in stochastic control theory (93E10) Stochastic stability in control theory (93E15)

Related Items (3)

Modeling and control of an agile tail-Sitter aircraft ⋮ Adaptive neural network sliding mode control for quad tilt rotor aircraft ⋮ Imaged-based visual servo control for a VTOL aircraft

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