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NASA NTRS ยท 19840012498

Space shuttle pilot-induced-oscillation research testing

Abstract

The simulation requirements for investigation of pilot-induced-oscillation (PIO) characteristics during the landing phase are discussed. Orbiters simulations and F-8 digital fly-by-wire aircraft tests are addressed.

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BibTeXRIS

Powers, B. G.. 1984-02-01. Space shuttle pilot-induced-oscillation research testing. https://ntrs.nasa.gov/citations/19840012498

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