AUTOPILOT FOR SYMMETRICAL ROLL-STABILIZED ROCKET Russian patent published in 1997 - IPC

Abstract RU 2085443 C1

FIELD: control system of symmetrical roll-stabilized rockets. SUBSTANCE: autopilot contains present flight speed sensor, threshold unit, controlled switch and two lateral-control channels including command setter, comparison unit, variable-gain factor amplifier, adder, integrator, angular-rate and transverse g-load sensors, modulus determination unit, scaler, comparator and servo actuator. EFFECT: enhanced accuracy of attitude control of rocket. 1 dwg

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RU 2 085 443 C1

Authors

Budilin V.A.

Godov B.G.

Kirillov P.M.

Krylov V.P.

Dates

1997-07-27—Published

1982-03-15—Filed