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(19)

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2 093 420

(13)

(51)

IPC

(21) (22)

Application

96110879/11, 1996-06-03

(22)

Actual filing date

1996-06-03

(45)

Published

1997-10-20

(72)

Inventor

Dzhandzhgava G.I.Gerasimov G.I.Verigo I.I.Kavinskij V.V.Kurdin V.V.Negrikov V.V.Orekhov M.I.

(73)

Holder

Ao Ramenskoe Priborostroitel'Noe Konstruktorskoe Bjuro

FLIGHT ALTITUDE CONTROL SYSTEM Russian patent published in 1997 - IPC

Abstract RU 2093420 C1

FIELD: aircraft instrumentation engineering; systems for control of flying vehicles in longitudinal plane. SUBSTANCE: system provides for required quality of control in closed control system at functional change in stabilization circuit parameters. System is additionally provided with two integrators connected in series, two multiplier units, division unit and three function generators. System provides for parametric stationarity of altitude closed control circuit and consequently satisfies quality of transient processes with no change in selected parameters of stabilization circuit. EFFECT: enhanced reliability. 1 dwg

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RU 2 093 420 C1

Authors

Dzhandzhgava G.I.

Gerasimov G.I.

Verigo I.I.

Kavinskij V.V.

Kurdin V.V.

Negrikov V.V.

Orekhov M.I.

Dates

1997-10-20—Published

1996-06-03—Filed