The paper presents an example of solving the parameter identification problem in case of platform with one degrees of freedom has been also presented. The parameter identification algorithm based on linear parameterization of the platform model and the least square criteria is developed. The desired derivatives of measured signals are estimated by means of designed differentiation filters. The required derivative order depends on the order of differential equations describing the object. The model was identified and verified using measurement results obtained for a real system.
The article presents the method of modeling the dynamics of a quadrocopter and presents a method for the selection of PID regulators. The quadrocopter's dynamics were derived based on the Lagrange equations of the second type. In the form of graphs, the simulation results were presented for the settings selected using the optimization method using the Wolfram Mathematica package
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