PIO I-II tendencies case study. Part 1. Mathematical modeling
In the paper, a study is performed from the perspective of giving a method to reduce the conservatism of the well known PIO (Pilot-Induced Oscillation) criteria in predicting the susceptibility of an aircraft to this very harmful phenomenon. There are three interacting components of a PIO – the pilo...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2010-03-01
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| Series: | INCAS Bulletin |
| Online Access: | http://bulletin.incas.ro/files/adrian_toader_v2no1_full.pdf |