-
DESIGN FEASIBILITY STUDY AND TECHNOLOGY DEMONSTRATION FOR DARAF ,MARKER ,BEACON, AUTO TAXING AND DIGITAL FLIGHT DATA RECORDER /
-
DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
-
DESIGN AND FABRICATION OF TSVU (TRI COPTER SHAPED VTOL UAV) /
-
DESIGN AND FABRICATION OF AIRFRAME STRUCTURE & CONTROLS OF UAV / Md. Fazlay Robbey, Md. Mukit Hasan, Saiful Islam .
-
DEVELOPMENT OF MICRO CONTROLLER BASED AVIONICS PACKAGE WITH REAL TIME FLIGHT VISUALIZATION EMERGENCY AUTO LANDING AND FLIGHT DATA RECORDER /
-
DESIGN AND FABRICATION OF AN UNMANNED AERIAL VEHICLE EATABLE OF DELIVERING MISSION PAYLOAD /
-
DESIGN AND FABRICATION OF A TARGET DRONE /
-
STUDY AND DESIGNING OF MICRO CONTROLLER BASED TEMPERATURE SENSING SYSTEM ALONG WITH GLOBAL SYSTEM FOR MOBILE INTERFACE AND ALARM MECHANISM TO BE USED IN EFFERENT TEMPERATURE SENSITIVE STOREHOUSES /
-
DESIGN AND FABRICATION OF A MICRO UAV WITH DEVELOPMENT OF ITS STRUCTURE, PROPULSION AND CONTROL SYSTEM / Md. Tauhid Rahman Evan, Mir Md. Al Kahman Tamal, Md. Jamal Mian
-
DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /
-
DESIGN AND FABRICATION OF LUNAR DUST EXCAVATOR ROBOT /
-
DESIGNING, DEVELOPMENT & FABRICATION OF SPRING MASS DAMPER SYSTEM /
-
DESIGN AND FABRICATION OF AUTOMATIC FUEL TRANSFER SYSTEM OF AN AIRCRAFT /
-
DESIGN,ANALYSIS AND FABRICATION OF A FULLY ARTICULATED HELICOPTER MAIN ROTOR SYSTEM /
-
DESIGN OF A CLOSED LOOP SUBSONIC WIND TUNNEL /
-
DESIGN S CONSTRUCTION OF A SUBSONIC OPEN LOOP WIND TUNNEL /
-
DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
-
DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.
-
DETECTION OF OBJECTS IN 2-D USING SONAR SENSOR /
-
DESIGN AND FABRICATION ON VACUUM ASSISTED INFUSIUN MOLDING SETUP FOR FABRICATION OF FLAT AND CURVED COMPOSITE PANELS /
-
PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
-
DATA FUSION OF IMU SENSORS AND ERROR REDUCTION USING KALMAN FILTER /
-
DESIGN PROTOTYPE PROPOSAL OF OPTICAL FIBER BASED AVIONICS DATA BUS FOR A SMALL AIRCRAFT / S.M. Easin Ankur, Faisal Ahmed & Akter Mahmud Nafi .
-
DESIGN AND IMPLEMENTATION OF A LAW COST ATTITUDE HEADING REFERENCE SYSTEM FOR LAW SPEED AIRCRAFT / Md. Shajid-Ul-Mahmud, Tariqul Islam, Md. Saiful Islam,