Ramesh, Gandham and Dwivedi, PN and Kumar, Naveen P and Padhi, R (2012) Effect of choice of basis functions in neural network for capturing unknown function for dynamic inversion control. In: Proceedings of National Systems Conference 2012, 2012, Annamalainagar, TN, India.Full text not available from this repository.
The basic requirement for an autopilot is fast response and minimum steady state error for better guidance performance. The highly nonlinear nature of the missile dynamics due to the severe kinematic and inertial coupling of the missile airframe as well as the aerodynamics has been a challenge for an autopilot that is required to have satisfactory performance for all flight conditions in probable engagements. Dynamic inversion is very popular nonlinear controller for this kind of scenario. But the drawback of this controller is that it is sensitive to parameter perturbation. To overcome this problem, neural network has been used to capture the parameter uncertainty on line. The choice of basis function plays the major role in capturing the unknown dynamics. Here in this paper, many basis function has been studied for approximation of unknown dynamics. Cosine basis function has yield the best response compared to any other basis function for capturing the unknown dynamics. Neural network with Cosine basis function has improved the autopilot performance as well as robustness compared to Dynamic inversion without Neural network.
|Item Type:||Conference Paper|
|Additional Information:||Copyright of this article belongs to Springer India.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||04 Mar 2014 11:32|
|Last Modified:||04 Mar 2014 11:32|
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