Flight control law design criteria for the transition phase for a tiltwing aircraft using multi-objective parameter synthesis

Author:

Holsten J.,Moormann D.

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference18 articles.

1. Fay, C.B.: A cursory analysis of the VTOL Tilt-Wing performance and control problems. Ann. NY. Acad. Sci. 107, 102–146 (1963)

2. Dickeson, J.J., Miles, D., Cifdaloz, O., Wells, V.L., Rodriguez, A.A.: Robust LPV H gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations. Am. Control. Conf. 2007, 5266–5271 (2007)

3. Oner, K.T., Ertugrul, C., Sirimoglu, E., Hancer, C., Ayken, T., Unel, M.: LQR and SMC stabilization of a new unmanned aerial vehicle. In: International Conference on Intelligent Control, Robotics, and Automation. Venice (2009)

4. Oner, K.T., Cetinsoy, E., Unel, M., Aksit, M.F., Kandemir, I., Gulez, K.: Dynamic model and control of a new quadrotor unmanned aerial vehicle with tilt-wing mechanism. Int. J. Appl. Sci Eng. Technol. 5, 2 (2009)

5. Ta, D.A., Fantoni, I., Lozano, R.: Modeling and control of a tilt tri-rotor airplane. Am. Control. Conf. 131(136), 27–29 (2012)

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