Stability margin-based PD attitude control tuning for unstable flight vehicle

DOI10.1080/00207721.2011.600471zbMath1307.93364OpenAlexW2057426977WikidataQ56945485 ScholiaQ56945485MaRDI QIDQ5172435

Ruiguang Yang, Mingwei Sun, Zeng-Qiang Chen, Zeng-Hui Wang

Publication date: 4 February 2015

Published in: International Journal of Systems Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207721.2011.600471

zbMATH Keywords

PD controltuningstability marginRouth stability criterion

Mathematics Subject Classification ID

Application models in control theory (93C95) Stability of control systems (93D99)

Related Items (3)

PID pitch attitude control for unstable flight vehicle in the presence of actuator delay: tuning and analysis ⋮ Proportional-derivative controllers for stabilisation of first-order processes with time delay ⋮ Improved PID controller design for unstable time delay processes based on direct synthesis method and maximum sensitivity

Cites Work

• Getting more phase margin and performance out of PID controllers
• Relay auto-tuning of PID controllers using iterative feedback tuning
• Tuning of PID controllers based on gain and phase margin specifications
• Satisfaction of gain and phase margin constraints using proportional controllers
• Gain margins and phase margins for control systems with adjustable parameters
• Stability robustness margin computation for structured real-parameter perturbations
• Adaptive PID control of systems with unknown time delay
• Controller Synthesis Free of Analytical Models: Three Term Controllers
• Design of stabilizing PI and PID controllers

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