FIELD: instrumentation engineering; determination of position coordinates and parameters of motion of flying vehicles launched from movable carriers.
SUBSTANCE: proposed navigation complex for flying vehicles has strap-down inertial navigational system, meter for measurement of carrier acceleration components and carrier angular-rate components, storage unit, computer for estimation of flying vehicle attitude angles relative to carrier and flying vehicle heading, roll and pitch computer. First input of storage unit is connected with output of meter of carrier acceleration components and angular-rate components. First input of heading, roll and pitch computer is connected with carrier attitude angle meter by means of carrier attitude angle data transmitting channel.
EFFECT: enhanced accuracy.
2 dwg
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