A flight control system for small unmanned aerial vehicle

DOI10.1007/s10778-018-0876-0zbMath1398.93249OpenAlexW2804424047MaRDI QIDQ1990917

A. A. Tunik, O. I. Nadsadnaya

Publication date: 26 October 2018

Published in: International Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10778-018-0876-0

zbMATH Keywords

static feedbackadaptationflight control\(H_\infty\)-controller

Mathematics Subject Classification ID

Feedback control (93B52) (H^infty)-control (93B36) Automated systems (robots, etc.) in control theory (93C85)

Related Items (2)

Synthesis of optimal feedback control of the crane-load system ⋮ Nonlinear control strategies for a UAV carrying a load with swing attenuation

Uses Software

• Aerosim

Cites Work

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• Static output feedback -- a survey
• On navigation sensor error correction
• Stability of the horizontal flight of an aircraft
• Robust control and \({\mathcal H}_{\infty}\)-optimization -- tutorial paper
• Synthesis of linear quadratic control laws on basis of linear matrix inequalities
• Gain-Scheduled Control via Switching of LTI Controllers and State Reset
• Linear Matrix Inequalities in System and Control Theory
• Stable LPV Realization of Parametric Transfer Functions and Its Application to Gain-Scheduling Control Design
• Static output feedback stabilization with H/sub /spl infin// performance for linear discrete-time systems
• Research on gain scheduling

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