CONTROL DEVICE FOR SYSTEM OF COORDINATED CONTROL OF FLIGHT VEHICLE Russian patent published in 2004 - IPC

Abstract RU 2237269 C1

FIELD: control devices for on-board automatic control systems of flight vehicles with an aircraft system with realization of capabilities of regimes with coordinated turns in the side channel with large bank angles.

SUBSTANCE: the control device has a roll-angle pick-off, roll-rate pick-off, first and second summing amplifiers, on-course control signal setter, first and second subtraction units, non-linear component with a dead band, sign inverter, dynamic unit for matching in dynamics of on-course and bank control signals, and a non-linear component with a limiter.

EFFECT: attained functional potentiality of variation of the intensity (level) of control in the roll channel in the conditions of load of the yaw channel, enhanced accuracy of control.

1 dwg

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RU 2 237 269 C1

Authors

Kravchuk S.V.

Puchkov A.M.

Syrov A.S.

Dates

2004-09-27Published

2003-04-03Filed