Geometric control using the state-dependent Riccati equation: application to aerial-acrobatic maneuvers

DOI10.1080/00207179.2021.1881165zbMath1497.93044OpenAlexW3128067204MaRDI QIDQ5095519

Jose Ángel Acosta, Saeed Rafee Nekoo, Aníbal Ollero

Publication date: 9 August 2022

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

Full work available at URL: https://zenodo.org/record/4616742

zbMATH Keywords

geometric controlquadcopteropen-loop optimal controlvariable-pitchflip maneuverSDDRE

Mathematics Subject Classification ID

Geometric methods (93B27) Automated systems (robots, etc.) in control theory (93C85) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (2)

Time-energy suboptimal control of nonlinear input-affine systems ⋮ Approximate optimal control design for quadrotors: A computationally fast solution

Cites Work

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• Exponential stability of an attitude tracking control system on SO(3) for large-angle rotational maneuvers
• Some discussions about the error functions on SO(3) and SE(3) for the guidance of a UAV using the screw algebra theory
• A geometric approach for quadrotor trajectory tracking control
• Nonlinear receding horizon control of an underactuated hovercraft
• SDRE based optimal finite-time tracking control of a multi-motor driving system
• Sliding mode control design based on the state-dependent Riccati equation: theoretical and experimental implementation

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