References
1. McRuer, D., Ashkenas, I., Graham, D. Aircraft Dynamics and Automatic Control. Princeton University Press; 1973.
2. Stevens, B., Lewis, F. Aircraft Control and Simulation. Wiley; 2003.
3. Etkin, B., Reid, L. Dynamics of Flight: Stability and Control. Wiley; 1996.
4. Mueller, T., DeLaurier, J., An Overview of Micro Air Vehicle Aerodynamics, vol. 195 of Progress in Aeronautics and Astronautics, chapter 1. , 2001:1–10. [Aiaa].
5. Bohorquez, F., Pines, D., Samuel, P. Small rotor design optimization using blade element momentum theory and hover tests. Journal of Aircraft. January-February 2010; 47(1):268–283.
6. Pesavento, U., Wang, Z. Flapping wing flight can save aerodynamic power compared to steady flight. Physical Review Letters ...
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