Stability augmentation for longitudinal modes of a small blended wing-body aircraft with canard as control surface / Rizal Effendy Mohd Nasir and Wahyu Kuntjoro
Failure to achieve satisfactory level for transient response of an aircraft in longitudinal motion - short period mode and phugoid modes - would mean poor flying and handling qualities leading to unnecessary pilot workload. This study proposes a stability augmentation system in longitudinal fly ing...
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Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM),
2013.
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A1234.567 |
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| Kopie 1 | Beschikbaar |