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ON SELECTION OF ZERO APPROXIMATION FOR THE ANGULAR POSITION OF AN ARTIFICIAL EARTH SATELLITE IN THE FORM OF TRIGONOMETRIC POLYNOMIALS TO THE FOURTH POWER
ON SELECTION OF ZERO APPROXIMATION FOR THE ANGULAR POSITION OF AN ARTIFICIAL EARTH SATELLITE IN THE FORM OF TRIGONOMETRIC POLYNOMIALS TO THE FOURTH POWER
FOR HIGH EARTH SATELLITES, THE SPECTRAL PRESENTATION FOR ANGLES OF ORIENTATION HAS COMPARATIVELY LARGE TERMS OF THE THIRD AND FOURTH POWER. SINCE IN ORIENTED MOTION THE SATELLITE, PROVIDED WITH A DAMPER, IS UNDER CONDITIONS OF FORCED OSCILLATION, THEN EVEN THE APPROXIMATING FORMULAS FOR THE ANGLES OF ORIENTATION CAN HAVE LARGE COEFFICIENTS WITH HARMONICS OF THE THIRD AND FOURTH POWER. RESEARCH CONDUCTED SHOWS THAT THE USE OF APPROXIMATING TRIGONOMETRIC POLYNOMIALS OF HIGH POWERS ALSO REQUIRES ADDITIONAL CONDITIONS WHICH ARE INDEPENDENT OF THE MAGNETOMETER READINGS.