Adaptive Control Using Neural Network for Command Following of Tilt-Rotor Airplane in 0 $^{\it 0}$ -Tilt Angle Mode

Author:

Im Jae Hyoung,Ha Cheolkeun

Publisher

Springer Berlin Heidelberg

Reference6 articles.

1. Harendra, P.B., Joglekar, M.J., Gaffey, T.M., Marr, R.L.: A Mathematical Model for Real Time Flight Simulation of the Bell Model 301 Tilt Rotor Research Aircraft. REPORT 301-099-001 (1973)

2. Baker, R.C., Charlie, B.: Nonlinear Unstable Systems. International Journal of Control 23(4), 123–145 (1989)

3. Troudet, T., Garg, S., Merrill, W.C.: Neural Network Application to Aircraft Control System Design. In: Proc. of AIAA Guidance, Navigation and Control Conference, vol. II, pp. 993–1009 (1991)

4. Kannan, S.K., Johnson, E.N.: Adaptive Trajectory Based Control for Autonomous Helicopters. In: AIAA Digital Avionics Conference, number 358, Irvine, CA (2002)

5. Yoon, H.S., Ha, C.K.: Robust Adaptive Nonlinear Control for Tilt-Rotor UAV. In: 2004 ICCAS International Conference on Control, Automation and Systems, Bangkok, Thailand, pp. 57–62 (2004)

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