TY - JOUR
T1 - Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems with Application to Hypersonic Flight Vehicle
AU - Xu, Bin
AU - Yang, Chenguang
AU - Pan, Yongping
N1 - Publisher Copyright:
© 2012 IEEE.
PY - 2015/10/1
Y1 - 2015/10/1
N2 - This paper studies both indirect and direct global neural control of strict-feedback systems in the presence of unknown dynamics, using the dynamic surface control (DSC) technique in a novel manner. A new switching mechanism is designed to combine an adaptive neural controller in the neural approximation domain, together with the robust controller that pulls the transient states back into the neural approximation domain from the outside. In comparison with the conventional control techniques, which could only achieve semiglobally uniformly ultimately bounded stability, the proposed control scheme guarantees all the signals in the closed-loop system are globally uniformly ultimately bounded, such that the conventional constraints on initial conditions of the neural control system can be relaxed. The simulation studies of hypersonic flight vehicle (HFV) are performed to demonstrate the effectiveness of the proposed global neural DSC design.
AB - This paper studies both indirect and direct global neural control of strict-feedback systems in the presence of unknown dynamics, using the dynamic surface control (DSC) technique in a novel manner. A new switching mechanism is designed to combine an adaptive neural controller in the neural approximation domain, together with the robust controller that pulls the transient states back into the neural approximation domain from the outside. In comparison with the conventional control techniques, which could only achieve semiglobally uniformly ultimately bounded stability, the proposed control scheme guarantees all the signals in the closed-loop system are globally uniformly ultimately bounded, such that the conventional constraints on initial conditions of the neural control system can be relaxed. The simulation studies of hypersonic flight vehicle (HFV) are performed to demonstrate the effectiveness of the proposed global neural DSC design.
KW - Dynamic surface control
KW - global stability
KW - hypersonic flight vehicle
KW - indirect and direct neural control
KW - smooth switching
KW - Strict-feedback system.
UR - http://www.scopus.com/inward/record.url?scp=84944036101&partnerID=8YFLogxK
U2 - 10.1109/TNNLS.2015.2456972
DO - 10.1109/TNNLS.2015.2456972
M3 - 文章
C2 - 26259222
AN - SCOPUS:84944036101
SN - 2162-237X
VL - 26
SP - 2563
EP - 2575
JO - IEEE Transactions on Neural Networks and Learning Systems
JF - IEEE Transactions on Neural Networks and Learning Systems
IS - 10
M1 - 7182323
ER -