Adaptive tuning of the fuzzy controller for robots
Fuzzy Sets and Systems
Nonlinear Control Systems
Notes on the approximation rate of fuzzy KH interpolators
Fuzzy Sets and Systems - Theme: Learning and modeling
Approximation properties of piece-wise parabolic functions fuzzy logic systems
Fuzzy Sets and Systems
Fuzzy process control: construction of control charts with fuzzy numbers
Fuzzy Sets and Systems
Mixed H2/H∞ fuzzy output feedback control design for nonlinear dynamic systems: an LMI approach
IEEE Transactions on Fuzzy Systems
Multilayer neural-net robot controller with guaranteed tracking performance
IEEE Transactions on Neural Networks
An adaptive H∞ controller design for bank-to-turn missiles using ridge Gaussian neural networks
IEEE Transactions on Neural Networks
Fuzzy basis functions, universal approximation, and orthogonal least-squares learning
IEEE Transactions on Neural Networks
H∞ reinforcement learning control of robot manipulators using fuzzy wavelet networks
Fuzzy Sets and Systems
Decentralized sliding mode control for bank-to-turn missile with backstepping technique
CAR'10 Proceedings of the 2nd international Asia conference on Informatics in control, automation and robotics - Volume 2
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This paper presents a novel mixed H2/H∞ autopilot design for bank-to-turn missiles. Based on sliding control theory, the proposed autopilot utilizes a fuzzy basis function network to approximate the unknown nonlinear functions of bank-to-.turn missile dynamics, enabling a mixed H2/H∞ controller with weight updating laws to be applied to attenuate the effects of approximation errors and external disturbances. Moreover, the mixed H2/H∞ autopilot design can minimize H2 performance criteria under a desired H∞ disturbance rejection constraint. Unlike general mixed H2/H∞ control problems, the proposed H2/H∞ autopilot with self-tuning fuzzy basis function network can avoid solving coupled Riccati equations by adequately selecting diagonal weighting matrices in the H2 performance criterion and H∞ constraint. Therefore, the proposed H2/H∞ control approach can be implemented efficiently. Computer simulation results are presented to illustrate the effectiveness of the proposed mixed H2/H∞ autopilot for BTT missiles.