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Rapid transfer alignment for tactical weapon applications
122
Citations
1
References
1989
Year
MissileEngineeringUliich Allows AlignmentRotational ManeuversSpacecraft Attitude ControlComputer-aided DesignDefence TechnologyRapid Transfer AlignmentCalibrationGuidance SystemNumerical SimulationSystems EngineeringKinematicsComputational GeometryGeometric ModelingAutomatic NavigationInertial SensorsAircraft NavigationMechatronicsComputer EngineeringDynamic PositioningTerminal BallisticsSatellite Navigation SystemsInertial Navigation SysreniAerospace EngineeringNatural Sciences
Inertial Navigation Sysreni (INS) concepts offer attractive benefits when applied to modern air-to-gro~~nd weapons because of countermeasures invulnerability, rapidly reducing size and cost and the ability to reduce the performance demands of terminal g~~ida i ice s ekers. Traditional INS transfer alignment methods place both time and maneuver constraints on tactical l a~mch timelines which detract from INS ~ ~ t i l i t y in tactical scenarios. A rapid transfer alignment approach is presented uliich allows alignment in less than ten seconds to an accuracy of less than one nirad w i t h o ~ ~ t the req~iirement for aircraft lateral plane maneuvers. The alignment approach augments the traditional nlasterislave velocity concept with masterlslave a t t i t ~ ~ d e matching wliich allows alignment error observability with rotational maneuvers. The resulting 24-state, 6-measurement Kalman filter is shown to be implementable using commercially available microprocessors with achieved filter update rates of 36 Hz.
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