Flight control system synthesis using eigenstructure assignment

DOI10.1007/BF00934464zbMath0518.93023OpenAlexW1973402993MaRDI QIDQ1054681

J. Blot

Publication date: 1984

Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00934464

zbMATH Keywords

output feedbackeigenstructure assignmentcontroller structural constraintsflight control systems

Mathematics Subject Classification ID

Pole and zero placement problems (93B55) Synthesis problems (93B50) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

• Unnamed Item
• Pole assignment by gain output feedback
• On the flexibility offered by state feedback in multivariable systems beyond closed loop eigenvalue assignment
• Eigenvalue/eigenvector assignment using output feedback
• Quadratic weights for asymptotic regulator properties

This page was built for publication: Flight control system synthesis using eigenstructure assignment