Majeed Mohamed

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The analysis of the aircraft model with aeroelastic interactions is extremely difficult task since the size of the flexible aircraft models is complex. This paper compares the model simplification methods to obtain low order mathematical model of a flexible aircraft, which is appropriate for control law design. In the present investigation, higher order(More)
In this paper, application of neural networks combined with partial differentiation of the neural outputs has been discussed to estimate lateral-directional flight stability and control parameter. A neural model capable of predicting generalized force and moment coefficients using measured motion and control variables can be employed to extract aerodynamic(More)
Wiener system is a block oriented model, having a linear time-invariant dynamic system followed by a memory-less nonlinearity. To design a stochastic estimator for online estimation of Wiener system of second order, this paper utilizes differential mean value theorem and the results of stochastic contraction theory. The asymptotic convergence of proposed(More)
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