The VEGA launcher atmospheric control problem: a case for linear parameter-varying synthesis

DOI10.1016/j.jfranklin.2021.07.057zbMath1481.93030OpenAlexW3198553034MaRDI QIDQ2071169

Andrés Marcos, Diego Navarro-Tapia, Samir Bennani

Publication date: 25 January 2022

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

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2021.07.057

zbMATH Keywords

\(\mathcal{H}_\infty\) controlleradaptive augmented designlinear parameter-varying synthesisVEGA launcher

Mathematics Subject Classification ID

Adaptive control/observation systems (93C40) (H^infty)-control (93B36) Linear systems in control theory (93C05)

Uses Software

• LPVTools

Cites Work

• Robust synthesis for linear parameter varying systems using integral quadratic constraints
• Robust performance of linear parametrically varying systems using parametrically-dependent linear feedback
• Parametric Robust Structured Control Design
• Linear, parameter-varying control and its application to a turbofan engine
• System analysis via integral quadratic constraints
• Survey of gain-scheduling analysis and design
• Legacy recovery and robust augmentation structured design for the VEGA launcher
• Nonsmooth H_∞Synthesis
• Induced L2-norm control for LPV systems with bounded parameter variation rates
• Research on gain scheduling