Abstract
Control of processing processes on the state of the spacecraft (SC) is represented by schemes of the invariant control loop of a complex dynamic object. Based on the analysis of the algorithms for estimating the parameters of the translational motion of an aircraft (LA), based on the results of external trajectory measurements, an iterative Gauss-Newton procedure is formulated that implements the approach of directly finding the extremal point of the response surface described by a multidimensional function. Applied to the problem of estimating the initial conditions of motion of an aircraft. The features of the implementation of the algorithm for estimating the initial conditions of the orbital motion of the apparatus based on the method of least squares are investigated.
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