Tripathi, Abha and Padhi, Radhakant (2008) A Neuro-Adaptive Approach for Robust Control of High Performance Aircrafts with Parameter Inaccuracies. In: National Systems Conference, IIT-Roorkee, IIT-Roorkee.
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For high performance aircrafts, the flight control system needs to be quite effective in both assuring accurate tracking of pilot commands, while simultaneously assuring overall stability of the aircraft. In addition, the control system must also be sufficiently robust to cater to possible parameter variations. The primary aim of this paper is to enhance the robustness of the controller for a HPA using neuro-adaptive control design. Here the architecture employs a network of Gaussian Radial basis functions to adaptively compensate for the ignored system dynamics. A stable weight mechanism is determined using Lyapunov theory. The network construction and performance of the resulting controller are illustrated through simulations with a low-fidelity six –DOF model of F16 that is available in open literature.
|Item Type:||Conference Paper|
|Keywords:||Flight control;Dynamic inversion;Neuro-Adaptive design;High performance aircrafts.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||29 Sep 2011 05:08|
|Last Modified:||29 Sep 2011 05:08|
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