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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Authors
Dates
1997-09-10—Published
1996-03-13—Filed