- Abstract
- Introduction
- Aircraft Equations of Motion
- Sliding Mode Based Reconfigurable Flight Control System Design
- Numerical Simulation

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https://www.riss.kr/link?id=A76340911
2003
English
SCIE,SCOPUS,KCI등재
학술저널
1-8(8쪽)
0
상세조회0
다운로드목차 (Table of Contents)
A Study on Assessment of Composite Couplings for Helicopter Rotor Blades with Multi-cell Sections
Wind Tunnel Test of the Straight and Forward Swept Canards
Recess Effects on Spray Characteristics of Swirl Coaxial Injectors
Virtual Flutter Flight Test of a Full Configuration Aircraft with Pylon/External Stores