iCLEAN â Loitering Attack UCAV - aero.com

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Deflection:To evaluate the results for the carbon wing, a stress factor wascalculated as followed:allowed carbon fiberallowed aluminum706.3270.82.6Thus, the maximal deflection of the wing:MaterialAluminumCarbonMax. Deflection[mm]62.324
WING'S FOLDING MECHANISMThe opening-wing and canard system:DESCRIPTION OF THE DISPLAYED SOLUTION1. The purpose is to design an opening set like the "Long Shot" by"Lockheed Martin" with a <strong>com</strong>bination of the popular"diamond back".2. The mechanism of the wing's opening is a stretched spring that hasbeen placed between the two wings. This slit is leaded by aconducted one.3. The process of opening the wing is fully automated duringlaunch time.The tracks move along with the wings until the UAV leaves thecanister. At that moment, the tracks fall and the wing openingsystem starts working automatically.4. During launch preparations, the wings are kept closed.25
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: ANALYSIS SIMULATIONA stress analysi
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 and 34: THE FULL ASSEMBLY OF THE MODELAs it
Page 35 and 36: The different configurations:OPENED
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