Nonlinear State Estimator Using the Data on Moving Horizon and its Application in the Problem of Spacecraft Attitudeстатья
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Аннотация:The possibility in principle of estimating the Euler−Krylov angles and projections of the angular velocity of a spacecraft by approximate data of incomplete measurements on the basis of the moving horizon method and non-linear estimator is considered. By means of numerical simulation a number of important properties of the method, including its robustness and conditions for stability, are established.