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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| Format: | Article |
| Language: | English |
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Faculty of Mechanical Engineering (FKM) and UiTM Press
2013
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| Online Access: | http://ir.uitm.edu.my/id/eprint/17579/ http://ir.uitm.edu.my/id/eprint/17579/2/AJ_RIZAL%20E.%20M.%20NASIR%20JME%2013.pdf |