FIELD: astronautics.
SUBSTANCE: proposed invention relates to stabilization method of structurally unstable carrier rocket oscillators using cruise or control engines. To stabilize oscillators, carrier rocket motion parameters are measured, stabilization algorithm based on use of a priori data on dynamic properties of carrier rocket, additional signal describing the unstable oscillator state, which is obtained based on its dynamics equation, is used.
EFFECT: providing asymptotic stability of fluid oscillators.
1 cl, 2 dwg
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