Publication Date:
2016-06-07
Description:
This presentation gives information on: pitch criteria based on airplane Bandwidth; apply research, experimental, operational data; compare Smith-Geddes, Gibson, Neal-Smith criteria; bandwidth criteria for Category II PIO; control/response sensitivity and PIO; extension to roll a axis; and some recommendations.
Keywords:
Aircraft Stability and Control
Type:
Pilot-Induced Oscillation Research: The Status at the End of the Century; Volume 1; 17-28; NASA/CP-2001-210389/VOL1
Format:
application/pdf
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