Design of attitude control system for UAV based on feedback linearization and adaptive control

DOI10.1155/2014/492680zbMath1407.93310OpenAlexW2026490188WikidataQ59067798 ScholiaQ59067798MaRDI QIDQ1718528

Wenya Zhou, Kuilong Yin, Rui Wang, Yue-E. Wang

Publication date: 8 February 2019

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2014/492680

Mathematics Subject Classification ID

Application models in control theory (93C95) Adaptive control/observation systems (93C40)

Related Items (1)

Stochastic Dynamics of Suspension System in Maglev Train: Governing Equations for Response Statistics and Reliability

Cites Work

• Adaptive support vector regression for UAV flight control
• Integrated guidance and autopilot design for a chasing UAV via high-order sliding modes
• A new delay system approach to network-based control
• High‐gain output feedback for a miniature UAV
• Adaptive backstepping flight control for a mini‐UAV

This page was built for publication: Design of attitude control system for UAV based on feedback linearization and adaptive control