Development of the Snapshot Method for Six Degree-of-Freedom Flight Dynamics Simulation of a High Aspect Ratio Wing Aircraft

Author:

Been Youngbeen,Kang Yoojin,Kim Seil,Shin Sangjoon,Jang Seyong

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference18 articles.

1. Drela M (1990) Method for simultaneous wing aerodynamic and structural load prediction. J Aircr 27(8):692–699

2. Brown E (2003) Integrated strain actuation in aircraft with highly flexible composite wings. Ph.D. Dissertation, Massachusetts Institute of Technology

3. Shearer C (2006) Coupled nonlinear flight dynamics, aeroelasticity, and control of very flexible aircraft. Ph.D. Dissertation, University of Michigan

4. Su W (2008) Coupled nonlinear aeroelasticity and flight dynamics of fully flexible aircraft. Ph.D. Dissertation, University of Michigan

5. Waszak MR, Schmidt DK (1988) Flight dynamics of aeroelastic vehicles. J Aircr 25(6):563–571

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