Aircraft navigation based on differentiation-integration observer
نویسندگان
چکیده
In this paper, a slimple linear high-gain integral-derivative observer is presented based on singular perturbation technique. The proposed integral-derivative observer can estimate synchronously the multiple integrals and derivatives of a signal. The merits of the presented integralderivative observer include its synchronous estimation of integrals and derivatives, simple implementation, sufficient stochastic noises rejection and almost no drift phenomenon. The theoretical results are confirmed by the frequency-domain analysis.
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