Optimal input design for aircraft stability and control flight testing

DOI10.1007/s10957-021-01912-0zbMath1481.90298OpenAlexW3212093857MaRDI QIDQ2055339

Eugene A. Morelli

Publication date: 1 December 2021

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

Full work available at URL: https://doi.org/10.1007/s10957-021-01912-0

zbMATH Keywords

parameter estimationoptimal input designaircraft stability and controlflight testing

Mathematics Subject Classification ID

Applications of mathematical programming (90C90) Sensitivity, stability, parametric optimization (90C31) System identification (93B30)

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Synthesis of test control for identification of aerodynamic characteristics of aircraft

Cites Work

• Control, identification, and input optimization
• An exact equivalence between the discrete- and continuous-time formulations of the Kalman filter
• Optimal input signals for parameter estimation in dynamic systems--Survey and new results
• Frequency-Domain Synthesis of Optimal Inputs for Linear System Parameter Estimation
• Optimal input design for aircraft parameter estimation