iCLEAN â Loitering Attack UCAV - aero.com

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PRINTING THE MODEL – THE RESULT OF THE PROCESSAfter fulfilling the instruction about the maximum size of a part,which led us “breaking” the model into parts (nose, body and tails,wings, canards) here are the results:Nose is being held by pressure, wings and canards are being held bysteel spacers and hinges. Also, steel reinforcements were inserted tothe wings and canards34
The different configurations:OPENED, CLOSED AND OPEN WITH TUFTS TEST MODELOPEN WING ONLY WITH TUFTS, BODY ONLY TEST MODEL35
Page 1 and 2: iCLEAN - Loitering Attack UCAV1
Page 5 and 6: MARKET SURVEYMARKET SURVEY - CONFIG
Page 8: PRELIMINARY DESIGNWORK PROCESSDivid
Page 12 and 13: After beginning with the first solu
Page 14 and 15: MOMENT VS. TIME FOR DIFFERENT BOOST
Page 16 and 17: PERFORMANCE CALCULATIONSMany and va
Page 18 and 19: WING DETAILED DESIGNWING ROOT JOINT
Page 21 and 22: Modeling of the wing-pivot connecti
Page 23 and 24: ANALYSIS SIMULATIONA stress analysi
Page 25 and 26: WING'S FOLDING MECHANISMThe opening
Page 27 and 28: TensionDragTension forces that appl
Page 29 and 30: FINAL CONFIGURATIONAs demonstrated
Page 31 and 32: WEIGHTS TABLEThe table below descri
Page 33: THE FULL ASSEMBLY OF THE MODELAs it
Page 37 and 38: The canard's lift coefficient isn't
Page 39 and 40: CONTROL SYSTEMSIMULINK MODELWe have
Page 41 and 42: [deg]RESULTSBy entering the coeffic
Page 43 and 44: u[ft/sec]0.02Project 086755 - 02997

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iCLEAN â Loitering Attack UCAV - aero.com