H∞ control of an overactuated tilt rotors quadcopter

Author:

Alkamachi AhmedORCID,Erçelebi Ergun

Publisher

Springer Science and Business Media LLC

Subject

Metals and Alloys,General Engineering

Reference40 articles.

1. Yeo H, Johnson W. Performance and design investigation of heavy lift tilt-rotor with aerodynamic interference effects [J]. Journal of Aircraft, 2009, 46(4): 1231–1239.

2. Çetinsoy E, Dikyar S, Hançer C, Oner K T, Sirimoglu E, Unel M, Aksit M F. Design and construction of a novel quad tilt-wing UAV [J]. Mechatronics, 2012, 22(6): 723–745.

3. Jeong S H, Jung S. Novel design and position control of an omni-directional flying automobile (Omni-flymobile) [C]// IEEE International Conference on Control Automation and Systems (ICCAS): 2010: 2480–2484.

4. Kendoul F, Fantoni I, Lozano R. Modeling and control of a small autonomous aircraft having two tilting rotors [C]// 44th IEEE Conference on Decision and Control. 2005: 8144–8149.

5. Öner K T, Çetinsoy E, Ünel M, Aksit M F, Kandemir I, Gülez K. Dynamic model and control of a new quadrotor unmanned aerial vehicle with tilt-wing mechanism [J]. World Academy of Science, Engineering and Technology, 2008, 2(9): 58–63.

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