iCLEAN â Loitering Attack UCAV - aero.com

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40alpha_aerogamau_dothqthetawuScope9Scope8Scope7Scope4Scope3Scope2Scope11s1s1s1s1s[w_dot][u_dot][gamma][alpha][alpha_aero][theta][h][q][V][delta_t][delta_e][theta_dot][h_dot][q_dot][w][u][alpha][theta][w][w][theta_dot][h_dot]-T-[gamma][u_dot][q][h][theta][u][w][q_dot][V][V][w_dot][u_dot]w_g
[deg]RESULTSBy entering the coefficient values as an assumption or by derived fromthe wind tunnel test, the simulation was running for a local level runs.We analyzed the control design by checking the step-response, onlooking the bode graphs to get the PM and GM:1.2Project 086755 – 029977584 – Mor Ram-On10.80.60.40.20-0.20 10 20 30 40 50 60 70 80 90 100Time[sec]STEP INPUT FOR As can be seen, in the sp, there is no steady state error for command.41
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 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: CONTROL SYSTEMSIMULINK MODELWe have
Page 43 and 44: u[ft/sec]0.02Project 086755 - 02997

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iCLEAN â Loitering Attack UCAV - aero.com