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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| Main Authors: | , |
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| Format: | Article |
| Language: | en |
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Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM)
2013
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| Subjects: | |
| Online Access: | https://ir.uitm.edu.my/id/eprint/17579/2/AJ_RIZAL%20E.%20M.%20NASIR%20JME%2013.pdf https://ir.uitm.edu.my/id/eprint/17579/ https://jmeche.uitm.edu.my/ |
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