NASA NTRS · 19670061426
Lateral stability augmentation of supersonic aircraft using multichannel optimal feedback control.
Abstract
Lateral stability augmentation of supersonic aircraft using linear multichannel state-vector optimal feedback control
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Bass, R. W., Stoner, J. W., Taylor, F. J.. 1966-01-22. Lateral stability augmentation of supersonic aircraft using multichannel optimal feedback control.. https://ntrs.nasa.gov/citations/19670061426
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