| 摘要 |
FIELD: control of two-stage missiles. SUBSTANCE: in the offered method of missile tracking, including measurement of flame coordinates and missile tracking in flame coordinates, measurement of optical transponder coordinates and missile tracking in optical transponder coordinates, constant measurement of missile model coordinates in missile flight time, missile tracking in flame coordinates is carried out after by the relation given in the description. Then, missile tracking is performed in model coordinates up to the measurement of optical transponder coordinates. EFFECT: enhanced reliability of tracking due to transition to inertia conditions of missile tracking before staging and appearance of signal from the optical transponder. |
