A unified approach to fixed-wing aircraft path following guidance and control

DOI10.1016/J.AUTOMATICA.2019.07.004arXiv1803.05184MaRDI QIDQ6119718

Claude Samson, J.-M. Kai, Tarek Hamel

Publication date: 20 February 2024

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://arxiv.org/abs/1803.05184

zbMATH Keywords

nonlinear control designpath-followinghardware-in-the-loop simulationfixed-wing aircraft

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Application models in control theory (93C95) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

• Nonlinear feedback control of axisymmetric aerial vehicles
• There is More than One Way to Frame a Curve
• Gain-scheduled bank-to-turn autopilot design using linear parameter varying transformations
• Introduction to feedback control of underactuated VTOLvehicles: A review of basic control design ideas and principles

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