FIELD: aviation.
SUBSTANCE: invention relates to the field of armaments, and specifically to the method and system of controlling flying apparatus, including those which rotate along the list angle as well as those which do not. According to the method for command formation in the initial moment of time, the already previously known values of the initial angle of the rocket's list and on the two mutually perpendicular planes with intersecting axis of the rocket are measured along with the magnetic poles of the Earth, which will determine the initial angle list. The value of the inaccuracy between the generic and the initial angle list of the rocket is measured and remembered. The current angle list of the rocket is summarised according to the magnetic field of the Earth with the value of the inaccuracy being taken into account of the resulting angle and gives of the signal of the list. On rockets rotating along the list angle, a magnetic sensor and a list angle compensator are installed and are joined with a master control for the initial list angle and computational device. The method proposes a means for correcting the list angle by which each of the two channels for both planes of control for the rocket create signals for their respective correction as first and second algebraic sums. The compensator for the list angle and each channel has a controlling inverter and two multipliers.
EFFECT: increased reliability and reduction of overall weight.
5 dwg
Title |
Year |
Author |
Number |
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