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 updated 15 days ago Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom equations of motion using MATLAB ODE sixdof(Forces, Moments, Mass, Inertia, tarray, varargin ) 4.29412 18 Ratings 11 Comments 77 Downloads (30 Days) updated 15 days ago Calculate aircraft variable-mass rigid-body six-degrees-of-freedom equations of motion using MATLAB sixdofvm(Forces, Moments, dMass, dInertia, tarray, vararg... 4.0 4 Ratings 7 Comments 34 Downloads (30 Days) updated 2 months ago Geoid Data for Aerospace Toolbox 0.0 0 Ratings 0 Comments 14 Downloads (30 Days) updated 10 months ago A set of functions for processing Mark Drela's AVL and XFoil data findValue(file, name, area) getSurfaceByName( Surfaces, name ) parseConfig( filename ) 4.5 2 Ratings 2 Comments 29 Downloads (30 Days) updated 1 year ago Finds Oswald efficiency factor for purposes of approximating a simple parabolic aircraft drag polar. oswaldfactor.m 5.0 1 Rating 0 Comments 25 Downloads (30 Days) updated 1 year ago EMPLOT generates an energy–maneuverability (E–M) plot. emplot(AC,h,n,v,Ps_contours,r_contours,n_contours) emplot_test.m 0.0 0 Ratings 1 Comment 21 Downloads (30 Days) updated 1 year ago Generates an airfoil shape using CST method CST_airfoil(wl,wu,dz,N); 5.0 1 Rating 1 Comment 22 Downloads (30 Days) updated 1 year ago Finds aircraft gross weight using the fuel fraction sizing method [FF, fracs]=missionfuelburn(varargin) breguet(type, task, E_R_or_frac, LD, SFC, V, eta_p) fuelfractionsizing(EWfunc,fixedW,FF,tol,maxW) 0.0 0 Ratings 0 Comments 20 Downloads (30 Days) updated almost 4 years ago Class interface between XFOIL and MATLAB, with the ability of running many instances in parallel. Airfoil XFOIL exampleXFOIL.m 5.0 7 Ratings 18 Comments 176 Downloads (30 Days) updated 4 years ago A VRML model of a wind turbine, animated with MATLAB and Simulink 3D Animation. (wind, farm, turbine) wind_turbine_code.m 4.75 4 Ratings 4 Comments 61 Downloads (30 Days) updated 4 years ago Several enhancements made to the original 747 demo. (fly, 747, matlab) terrain_plane.m 0.0 0 Ratings 4 Comments 44 Downloads (30 Days) updated 4 years ago Animate the motion of a 747 along a helical path all from within MATLAB. (aerospace, 747, 3d) Plane_Helix.m 5.0 1 Rating 3 Comments 51 Downloads (30 Days) updated 4 years ago Special effects added algorithmically terrain_plane.m 3.0 1 Rating 3 Comments 18 Downloads (30 Days) updated 5 years ago The Aircraft Library [CD,CL,CY,Cl,Cm,Cn]=ab2dv(Alg,Blg,Alt,Blt,GM,deltaE_0,alp... [X0,U0]=air3m(name,V,H,G) demos 4.0 5 Ratings 5 Comments 92 Downloads (30 Days) updated 5 years ago Generates the NACA 5 digit airfoil coordinates naca5gen(iaf) tst_naca5gen.m 0.0 0 Ratings 2 Comments 57 Downloads (30 Days) updated almost 6 years ago Generates the NACA 4 digit airfoil coordinates naca4gen(iaf) tst_naca4gen.m 4.4 5 Ratings 2 Comments 198 Downloads (30 Days) updated almost 6 years ago DRAW SIMPLE AIRCRAFT WITH VARIABLE PARAMETERS EGAB(varargin) 0.0 0 Ratings 0 Comments 26 Downloads (30 Days) updated 7 years ago Wing Designer computes aircraft performance measures from wing and engine parameters. DeterminePanelGeometry(inputgeo, figs) DetermineProfileDrag(airfoildata,geo,panel) FinalOutput(CL, CDi, CD0, y_cp, geo, WingVolume, airfoild... 5.0 2 Ratings 1 Comment 56 Downloads (30 Days) updated 10 years ago Sink the computer's battleships in as few moves as possible. 2.66667 3 Ratings 2 Comments 38 Downloads (30 Days) updated 10 years ago This function plot in the same figure the center trajectory and attitude of an aircraft. trajectory2(x,y,z,pitch,roll,yaw,scale_factor,step,vararg... 4.75 4 Ratings 6 Comments 36 Downloads (30 Days) updated 11 years ago 1903 Wright Flyer modeled with Simulink, Aerospace Blockset and Virtual Reality Tool. aeroblk_wf_3dof_data.m aeroblk_wf_3dof aeroblk_wf_3dof_R13 3.66667 3 Ratings 3 Comments 25 Downloads (30 Days) updated 12 years ago Virtual Reality toolbox interface for airplanes. aero2vr 4.0 3 Ratings 3 Comments 12 Downloads (30 Days) updated 12 years ago Companion Software [FD,GD,AD,ND,BD]=cvrt(F,G,A,N,B,TS) [FD,GD,AD,ND,BD]=cvrt(F,G,A,N,B,TS) [FD,GD,SC,RMSY,RMSU,EV]=mimodcom(F,G,HY,A,N,B,GA,H,Q,V,T) 5.0 1 Rating 2 Comments 25 Downloads (30 Days) updated 13 years ago Performance of a Cessna Excel Model 560 XL aceqs(t,x) aceqs(t,x) aceqs(t,x) 3.0 2 Ratings 0 Comments 25 Downloads (30 Days)

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