DESIGN AND DEVELOPMENT OF INERTIAL MEASURMENT UNIT (IMU) IN ATTITUDE HEADING REFERENCE SYSTEM (AHRS) FOR REAL TIME MANEUVER MONITORING OF LOW ALTITUDE AIRCRAFT BY USING KALMAN FILTER /

Míreanna comhchosúla

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• DATA FUSION OF IMU SENSORS AND ERROR REDUCTION USING KALMAN FILTER /
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• GPS-INS NEWLY PROPOSED INTEGRATED SYSTEM BASED ON KALMAN FILTER AND COMPLEMENTARY FILTER FOR AIRCRAFT POSITION DETERMINATION /
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• DESIGN AND IMPLEMENTATION OF A LAW COST ATTITUDE HEADING REFERENCE SYSTEM FOR LAW SPEED AIRCRAFT / Md. Shajid-Ul-Mahmud, Tariqul Islam, Md. Saiful Islam,
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• Modern inertial sensors and systems /
  de réir: Bose, Amitava
  Foilsithe / Cruthaithe: (2008)