PID pitch attitude control for unstable flight vehicle in the presence of actuator delay: tuning and analysis

DOI10.1016/j.jfranklin.2014.09.013zbMath1393.93110OpenAlexW2074137041WikidataQ56945409 ScholiaQ56945409MaRDI QIDQ1660386

Zenqiang Chen, Mingwei Sun, Li-Min Zhang, Zeng-Hui Wang

Publication date: 16 August 2018

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2014.09.013

zbMATH Keywords

increasing gain and phase margins (iGPM)PID pitch attitude controlunstable flight vehicle

Mathematics Subject Classification ID

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

Related Items (1)

Echo state network based predictive control with particle swarm optimization for pneumatic muscle actuator

Cites Work

• Automatic tuning of simple regulators with specifications on phase and amplitude margins
• Nonlinear robust control for reusable launch vehicles in reentry phase based on time-varying high order sliding mode
• Tuning of PID controllers based on gain and phase margin specifications
• Launch vehicle attitude control using sliding mode control and observation techniques
• Flight Control System Design with Rate Saturating Actuators
• Stability robustness margin computation for structured real-parameter perturbations
• Stability margin-based PD attitude control tuning for unstable flight vehicle

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