This study proposes a low-computational composite adaptive neural control scheme for the longitudinal dynamics of a swept-back wing aircraft subject to parameter uncertainties. To efficiently release the constraint often existing in conventional neural designs, whose cl... View more
Yue, T., Wang, L., Ai, J.. Gain self-scheduled H∞ control for morphing aircraft in the wing transition process based on an LPV model.
Chinese Journal of Aeronautics. 2013; 26 (4): 909-917
Wang, T., Dong, C., Wang, Q.. Finite-time boundedness control of morphing aircraft based on switched systems approach.
Optik. 2015; 126 (23): 4436-4445
Wu, Z., Lu, J., Zhou, Q., Shi, J.. Modified adaptive neural dynamic surface control for morphing aircraft with input and output constraints.
Nonlinear Dynamics. 2017; 87 (4): 2367-2383
Baldelli, D. H., Lee, D.-H., Sánchez Peñal, R. S., Cannon, B.. Modeling and control of an aeroelastic morphing vehicle.
Journal of Guidance, Control, and Dynamics. 2008; 31 (6): 1687-1699
Wu, Z., Lu, J., Rajput, J., Shi, J., Ma, W.. Adaptive neural control based on high order integral chained differentiator for morphing aircraft.
Mathematical Problems in Engineering. 2015; 2015: 1-12
Jiang, W., Dong, C., Wang, Q.. A systematic method of smooth switching LPV controllers design for a morphing aircraft.
Chinese Journal of Aeronautics. 2015; 28 (6): 1640-1649
Wang, D., Huang, J.. Neural network-based adaptive dynamic surface control for a class of uncertain nonlinear systems in strict-feedback form.
IEEE Transactions on Neural Networks. 2005; 16 (1): 195-202
Zou, A.-M., Hou, Z.-G., Tan, M.. Adaptive control of a class of nonlinear pure-feedback systems using fuzzy backstepping approach.
IEEE Transactions on Fuzzy Systems. 2008; 16 (4): 886-897
Kim, B. S., Yoo, S. J.. Approximation-based adaptive control of uncertain non-linear pure-feedback systems with full state constraints.
IET Control Theory & Applications. 2014; 8 (17): 2070-2081
Shen, Q., Jiang, B., Cocquempot, V.. Fuzzy logic system-based adaptive fault-tolerant control for near-space vehicle attitude dynamics with actuator faults.
IEEE Transactions on Fuzzy Systems. 2013; 21 (2): 289-300