COMPLEX INERTIAL SYSTEM Russian patent published in 1997 - IPC

Abstract RU 2089450 C1

FIELD: flying vehicle navigation and attitude systems. SUBSTANCE: complex inertial system includes "n" angular-rate sensor units, navigation and attitude parameters shaping unit; "m" linear acceleration sensor units; "n" angular velocity filters; "m" linear acceleration filters and two information processing units. EFFECT: enhanced accuracy. 2 cl, 3 dwg

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RU 2 089 450 C1

Authors

Dzhandzhgava G.I.

Budkin V.L.

Gerasimov G.I.

Negrikov V.V.

Rogalev A.P.

Dates

1997-09-10Published

1996-03-13Filed