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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, CONSTRUCTION AND PERFORMANCE CHECKING OF A LOW COST & LIGHTER BLADE ANTENNA /
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DEVELOPMENT OF INTERACTIVE MULTIMEDIA PACKAGE ON AIRCRAFT INSTRUMENTS / Flg offr Mosammat Samia Khanam, Flg offer Shariaz Ebna Khalam, Md. Rashed Hossain
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DESIGN, ANALYSIS AND OPTIMIZATION OF A SMALL UNMANNED AIRCRAFT /
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DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
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SURFACE MODIFICATION OF NACA 4418 AIRFOIL WITH DIFFERENT SHAPED DIMPLES AND AERODYNAMIC PERFORMANCE ANALYSIS /
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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 /
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MODIFICATION OF A TURBO-JET ENGINE (F-7 ENGINE) AS A TRAINING AID / Flg offr A.K.M.Tajul Islam, Flg offr Md. Sayed Jaber, Flg offr B.M.Anisuzzaman
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A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
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DESIGN FEASIBILITY STUDY AND TECHNOLOGY DEMONSTRATION FOR DARAF ,MARKER ,BEACON, AUTO TAXING AND DIGITAL FLIGHT DATA RECORDER /
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DESIGN AND FABRICATION OF AUTOMATIC FUEL TRANSFER SYSTEM OF AN AIRCRAFT /
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DESIGN OF MINIATURE TYPE PARALLEL COUPLED MICRO STRIP HAIR PIN FILTER IN VHF /
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STUDY OF GNSS AND ANALYSIS OF ITS IMPROVEMENT FOR POSITIONING ACCURACY /
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DATA FUSION OF IMU SENSORS AND ERROR REDUCTION USING KALMAN FILTER /
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A SYSTEMS ENGINEERING APPROACH TO THE DETAIL DESIGN OF TAIL,TRIM AND PERFORMANCE ANALYSIS OF A SMALL REMOTELY PILOTED AIRCRAFT /
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DESIGN AND DEVELOPMENT OF A BLADE ANTENNA FOR AIRCRAFT NAVIGATION AND COMMUNICATION /
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ANALYSIS OF OPERATIONAL LIMIT OF AN AIRCRAFT: AN AEROELASTIC APPROACH /
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A STUDY OF ELECTRONIC NAVIGATION SYSTEM AND OPTICAL INSTRUMENTS /
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DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
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DESIGN AND DEVELOPMENT OF MFD PAGES FOR FIGHTER AIRCRAFT USING FLIGHTGEAR FLIGHT SIMULATOR DATA OUTPUT /
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DEVELOPMENT OF A PHASED OUT AIRCRAFT AS EDUCATIONAL AID /
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DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.
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DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
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DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /