Application of real/mixed μ computational techniques to anH∞ missile autopilot

DOI<link itemprop=identifier href="https://doi.org/10.1002/(SICI)1099-1239(199610)6:8<743::AID-RNC187>3.0.CO;2-O" /><743::AID-RNC187>3.0.CO;2-O 10.1002/(SICI)1099-1239(199610)6:8<743::AID-RNC187>3.0.CO;2-OzbMath0857.93066OpenAlexW2333251362MaRDI QIDQ4717513

G. Ferreres, Vincent Fromion, Gilles Duc, Mohammed M'Saad

Publication date: 26 February 1997

Full work available at URL: https://doi.org/10.1002/(sici)1099-1239(199610)6:8<743::aid-rnc187>3.0.co;2-o

zbMATH Keywords

robust stabilitystructured singular valuemissile autopilot\(H_ \infty\)parametric aerodynamic uncertainties

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Application models in control theory (93C95) Free motion of a rigid body (70E15)

Related Items (1)

Robust controller order reduction

This page was built for publication: Application of real/mixed μ computational techniques to anH∞ missile autopilot