Flying qualities based time-varying stability augmentation system design for tiltrotor conversion control

Author:

WANG Chen,TAN Wenqian,SUN Liguo,JIAO JunkaiORCID

Funder

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Reference36 articles.

1. Foster M. The future evolution of the tiltrotor. Reston: AIAA; 2003. Report No.: AIAA-2003-2652.

2. Modelling and control of mini-flying machines;Castillo;IEEE Contr Syst,2006

3. Viganò L, Riccardi F, Leonello D. Development of augmented control laws for a tiltrotor in low and high speed flight modes. In: 43rd European rotorcraft forum. Red Hook: Curran Associates, Inc; 2018. p. 438–51.

4. Malpica CA, Decker WA, Theodore CR, et al. An investigation of large tilt-rotor hover and low speed handling qualities. In: The American helicopter society 67th annual forum. West Palm Beach: AHS; 2011. p. 1386–404.

5. Yu L, Zhang DB, Zhang JY. Transition flight modeling and control of a novel tilt tri-rotor UAV. In: 2017 IEEE international conference on information and automation (ICIA). Piscataway: IEEE Press; 2017. p. 983–8.

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