Output Error Method for Tiltrotor Unstable in Hover
This article investigates unstable tiltrotor in hover system identification from flight test data. The aircraft dynamics was described by a linear model defined in Body-Fixed-Coordinate System. Output Error Method was selected in order to obtain stability and control derivatives in lateral motion. F...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Polish Academy of Sciences
2017-03-01
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| Series: | Archive of Mechanical Engineering |
| Subjects: | |
| Online Access: | http://www.degruyter.com/view/j/meceng.2017.64.issue-1/meceng-2017-0002/meceng-2017-0002.xml?format=INT |