DocumentCode
697670
Title
Lateral auto-pilot design for an agile missile using dynamic fuzzy neural networks
Author
Er, M.J. ; Gao, Y. ; Leithead, W.E. ; Leith, D.J.
Author_Institution
Sch. of Electr. & Electron. Eng., Nanyang Technol. Univ., Singapore, Singapore
fYear
2001
fDate
4-7 Sept. 2001
Firstpage
3911
Lastpage
3916
Abstract
This paper presents a new approach, which exploits the recently developed Dynamic Fuzzy Neural Networks (DFNN) learning algorithm. The DFNN is based on extended Radial Basis Function (RBF) neural networks, which are functionally equivalent to Takagi-Sugeno-Kang (TSK) fuzzy systems. The algorithm comprises 4 parts: (1) Criteria of rules generation; (2) Allocation of premise parameters; (3) Determination of consequent parameters and (4) Pruning technology. The salient characteristics of the approach are: (1) A hierarchical on-line self-organizing learning paradigm is employed so that not only parameters can be adjusted, but also the determination of structure can be self-adaptive without partitioning the input space a priori; (2) Fast learning speed can be achieved so that the system can be implemented in real time. The application of the proposed approach is demonstrated in application to a demanding, highly nonlinear, missile control design task. Scheduling on instantaneous incidence (a rapidly varying quantity) is well known to lead to considerable difficulties with classical gain-scheduling methods. It is shown that the methods proposed here can, however, be used to successfully design an effective intelligent controller.
Keywords
fuzzy control; fuzzy neural nets; fuzzy systems; learning systems; missile control; neurocontrollers; radial basis function networks; scheduling; self-adjusting systems; DFNN learning algorithm; RBF neural network; TSK fuzzy system; Takagi-Sugeno-Kang fuzzy system; agile missile; classical gain-scheduling method; consequent parameter determination; dynamic fuzzy neural networks learning algorithm; extended radial basis function neural network; instantaneous incidence; intelligent controller; lateral auto-pilot design; learning speed; missile control design task; online self-organizing learning paradigm; premise parameter allocation; pruning technology; rules generation criteria; salient characteristics; self-adaptive without partitioning; Acceleration; Aerodynamics; Aerospace control; Equations; Fuzzy control; Heuristic algorithms; Missiles;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (ECC), 2001 European
Conference_Location
Porto
Print_ISBN
978-3-9524173-6-2
Type
conf
Filename
7076545
Link To Document