METHOD OF A ROCKET CONTROL Russian patent published in 2005 - IPC

FIELD: rocketry; methods of a rocket control.

SUBSTANCE: the invention is pertaining to the field of rocketry, in particular, to the rocket control methods and may be used in the rocket complexes of the telecontrolled rockets. The technical result is prevention of an overlapping of the optical communication lines "a carrier - a rocket" and "a carrier - a target" by a smoke tails from the own rocket accelerating engine. The substance of the invention consists that they form and store the signal of the program angular speed of motion of the longitudinal axis of the rocket under action of gravity at the horizontal level of a target sight line. Measure the angular speed of the rocket longitudinal axis motion. Determine a threshold value of an error between the signal of the running measured angular speed of the rocket longitudinal axis and the stored signal of the program angular speed, which corresponds to the running time of the flight. Before the rocket lock-on the target for tracking compare the signal of the measured angular rate of the longitudinal axis of the rocket with the program stored signal of the angular speed of the longitudinal axis of the rocket corresponding to the running time of the rocket flight and, if an error between these signals exceeds the fixed threshold value, then give the rocket longitudinal axis an additional angular speed of motion equal to the value of the difference between the corresponding running time of the rocket flight angular rate of a longitudinal axis of a ROCKET signal stored by the program and the signal of angular speed of the rocket longitudinal axis measured.

EFFECT: the invention ensures prevention of an overlapping of the optical communication lines "a carrier - a rocket" and "a carrier - a target" by a smoke tails from the own rocket accelerating engine.

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