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NASA NTRS · 19660022830

Bending feedback control Final report

Waymeyer, W. K.

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Abstract

Application of quadratic optimal control, least squares state, and parameter estimation to stability and control of flexible launch vehicle

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OPTIMAL CONTROL LAUNCH VEHICLE STABILITY AND CONTROL LEAST SQUARES METHOD

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Waymeyer, W. K.. 1966-06-01. Bending feedback control Final report. https://ntrs.nasa.gov/citations/19660022830

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