Longitudinal command stability augmentation system design for unstable aircraft using flying and handling qualities specifications
This paper demonstrates a practical approach in designing a longitudinal command stability augmentation system for unstable combat aircraft. The unaugmented aircraft is originally unstable configuration in order to gain fast response for agility. The flight control system was designed in compliance...
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| Main Authors: | , , |
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| Format: | Conference or Workshop Item |
| Published: |
Institute of Electrical and Electronics Engineers Inc.
2016
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| Subjects: | |
| Online Access: | http://eprints.utm.my/id/eprint/73472/ https://www.scopus.com/inward/record.uri?eid=2-s2.0-84965113448&doi=10.1109%2fICCNEEE.2015.7381444&partnerID=40&md5=caeb593da684ba442000569b9a90702c |
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