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2 090 462

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C1

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IPC

(21) (22)

Application

4516957/11, 1989-06-28

(22)

Actual filing date

1989-06-28

(45)

Published

1997-09-20

(72)

Inventor

Temnov I.I.

(73)

Holder

Nauchno-Proizvodstvennoe Ob"Edinenie Im.S.A.Lavochkina

METHOD OF STABILIZATION OF SPACE VEHICLE WITH COMBINED GYRO-INERTIAL AND JET ACTUATORS Russian patent published in 1997 - IPC

Abstract RU 2090462 C1

FIELD: stabilization of space vehicles. SUBSTANCE: method consists in measurement of angle of deflection and angular velocity of space vehicle from preset values, forming alternating control moment proportional to sum of measured deflections when this sum exceeds preset value. Alternating control moment is formed through acceleration and deceleration of gyro-inertial actuators to zero rotational speedy In case deflection of angular velocity exceeds preset value, control moment is formed in function of measured deflection on jet actuators. EFFECT: enhanced reliability.

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RU 2 090 462 C1

Authors

Temnov I.I.

Dates

1997-09-20—Published

1989-06-28—Filed

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