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...
Saved in:
Main Authors: | , |
---|---|
Format: | Article |
Language: | English |
Published: |
Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM)
2013
|
Subjects: | |
Online Access: | http://ir.uitm.edu.my/id/eprint/17579/2/AJ_RIZAL%20E.%20M.%20NASIR%20JME%2013.pdf http://ir.uitm.edu.my/id/eprint/17579/ https://jmeche.uitm.edu.my/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|