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DESIGN AND APPLICATION OF DISCRETE EXTENDED KALMAN FILTER IN INERTIAL NAVIGATION SYSTEM STRAP DOWN TYPE ON RKX-200 ROCKET USING MAGNETOMETER, ALTIMETER AND GPS AS CORRECTOR

DESIGN AND APPLICATION OF DISCRETE EXTENDED KALMAN FILTER IN INERTIAL NAVIGATION SYSTEM STRAP DOWN TYPE ON RKX-200 ROCKET USING MAGNETOMETER, ALTIMETER AND GPS AS CORRECTOR

by NUGROHO (NIM : 13311041); SYARIF HIDAYATULLAH (NM : 13311083); , HARIO

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