Control-oriented modeling of a high-aspect-ratio flying wing with coupled flight dynamics

Author:

NIU Cong,YAN Xiutian,CHEN Boyi

Funder

Fundamental Research Funds for the Central Universities

National Natural Science Foundation of China

Natural Science Foundation of Jiangsu Province

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference34 articles.

1. A review on non-linear aeroelasticity of high aspect-ratio wings;Afonso;Prog Aeros Sci,2017

2. Noll T, Brown J, Perez-Davis M, et al. Investigation of the Helios prototype aircraft mishap volume I mishap report; 2004. Washington, D.C.: NASA Langley Research Center; Report No.: 64317.

3. Aeroelastic analysis of composite wings;Cesnik,1996

4. Aeroelastic characteristics of a highly flexible aircraft;van Schoor;J Aircr,1990

5. Aeroelastic effects of battens on the flight dynamics of a MAV;Babcock,2012

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