СПОСОБ ФОРМИРОВАНИЯ ПРОГРАММЫ ОРИЕНТАЦИИ РАЗГОННОГО БЛОКА ПРИ ТЕРМИНАЛЬНОМ УПРАВЛЕНИИ ЕГО НАВЕДЕНИЕМ НА ЗАДАННУЮ ОРБИТУ

摘要

FIELD: terminal control of motion trajectory of cryogenic stages injecting spacecraft into preset orbits by means of cruise engines. ^ SUBSTANCE: swivel combustion chamber of cruise engine is used for angular orientation and stabilization of cryogenic stage of spacecraft. Proposed method includes predicting parameters of motion of cryogenic stage at moment of cut-off of cruise engine; deviation of radius and radial velocity from preset magnitudes are determined; angle of pitch and rate of pitch are corrected and program of orientation of thrust vector for subsequent interval of terminal control is determined. By projections of measured phantom accelerations, angle of actual orientation of cruise engine thrust vector and misalignment between actual and programmed thrust orientation angles are determined. This misalignment is subjected to non-linear filtration, non-linear conversion and integration. Program of orientation of cryogenic stage is determined as difference between programmed thrust orientation angle and signal received after integration. Proposed method provides for compensation for action of deviation of cruise engine thrust vector relative to longitudinal axis of cryogenic stage on motion trajectory. ^ EFFECT: enhanced accuracy of forming preset orbit. ^ 5 dwg, 1 tbl