Design of robust controller of fixed-wing UAV for transition flight

2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014 - Conference Proceedings

Volumn , Issue , 2014, Pages 1111-1116

  Kohno, Satoshi ^a   Uchiyama, Kenji ^a  

^a NIHON UNIVERSITY   (Japan)

Author keywords

DAC observer; dynamic inversion method; fixed wing UAV; transition flight

Indexed keywords

AIRCRAFT; CONTROL SYSTEMS; FIXED WINGS;

DAC OBSERVER; DESIGN OF ROBUST CONTROLLERS; DISTURBANCE ACCOMMODATING CONTROLS; DYNAMIC INVERSION; EQUILIBRIUM TRANSITIONS; FLIGHT CONTROL DESIGN; TRANSITION FLIGHT; TRANSLATIONAL MOTIONS;

FLIGHT CONTROL SYSTEMS;

EID: 84904573749     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICUAS.2014.6842364     Document Type: Conference Paper

References (8)

1. K. Muraoka, N. Okada, and D. Kubo, "Quad Tilt Wing VTOL UAV: Aerodynamic Characteristics and Prototype Flight Test," AIAA, Unm nned...Unlimi ed C nferen e, 9, AIAA-2009-1834.
2. J. H. Lee, B. M. Min, and E. T. Kim, "Autopilot Design of Tilt-rotor UAV Using Particle Swarm Optimization Method, International Conference on Control," Automation and Systems, 2007, pp.1629-1633.
3. V. Myrand-Lapierre, A. Desbiens, E. Gagnon, F. Wong, and E. Poulin, "Trniin Beween Level Flighnd Hveringfr Fixed-Wing Mini Aerial Vehicle," Preeding the Amerin Cnrl Conference, 2010, pp.530-535.
4. Y. Akai, Y. Shimada, K. Uchiyama, and A. Abe,."Design of Nonlinear Attitude Control System for Spaceplane Using Disturbance-Accommodating Control," Proceedings of KSAS-JSASS Joint International Symposium on Aerospace Engineering, 2008, pp.542-547.
5. C. D. Johnson, "A Fmily f "Univer l Ad p ive Cnrller " f r Linear and Nonlinear Plants," Proceedings of the Twentieth Southeastern Symposium on System Theory, 1988, pp.530-534.
6. R. Giroux, R. Gourdeau, and R. Landry, "Extended Kalman Filter Implementation for Lo-cost INS/GPS Integration in a Fast Prototyping Environment," 16th Symposium on Navigation of the Canadian Navigation society, 2005, pp.1-11.
7. M. Kokume and K. Uhiym , "Cnrl Arhieure f r Trniin between Level Flight to Hovering of a Fixed-Wing UAV," Jurnlf JSASS, Vol.60, 2012, pp173-180. (in Japanese)
8. K. Iwasaki and K. Uchiyama "Robust Controller Design for Transition Flight for Fixed-Wing UAV," Proceedings of Asia-Pacific International Symposium on Aerospace Technology (APISAT), 2012, CD-ROM 7.5.2.