Flight control design using robust dynamic inversion and time-scale separation

DOI10.1016/S0005-1098(96)00101-XzbMath0871.93037OpenAlexW2142592419MaRDI QIDQ5961498

Gary J. Balas, William L. Garrard, Jacob Reiner

Publication date: 7 October 1997

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0005-1098(96)00101-x

zbMATH Keywords

time-scale separationfeedback linearizationrobust nonlinear flight controllersstructured singular value

Mathematics Subject Classification ID

Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51) Time-scale analysis and singular perturbations in control/observation systems (93C70)

Related Items

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Uses Software

• Mu Analysis and Synthesis Toolbox

Cites Work

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• The complex structured singular value
• State-space solutions to standard H/sub 2/ and H/sub infinity / control problems
• High performance linear-quadratic and H-infinity designs for a 'supermaneuverable' aircraft
• Nonlinear control law with application to high angle-of-attack flight
• High-alpha application of variable-gain output feedback control
• Nonlinear feedback control of highly manoeuvrable aircraft