% INITIAL CONDITIONS FOR THE SYSTEM % For the MC column below: % MC=0: not a random variable % MC=1: uniform distribution % MC=2: gaussian distribution % %========================================================================================= % SIMULATION PARAMETERS %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 1 0.0 0 0 % s | time: simulation time 2 0.0 0 0 % s | dt: simulation dt 3 0.1 0 0 % s | dtout: output time step 4 30.0 0 0 % s | endTime: simulation stop time 5 1.0 0 0 % n/a | index: step number for sync %========================================================================================= % FLIGHT SECTION %========================================================================================= %========================================================================================= % FLIGHT::DYNAMICS %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 10 0 0 0 % m | fdX: x position 11 0 0 0 % m | fdY: y position 12 900 0 0 % m | fdZ: z position 13 0 0 0 % m/s | fdVXE: vxe velocity 14 0 0 0 % m/s | fdVYE: vye velocity 15 0 0 0 % m/s | fdVZE: vze velocity 16 0 0 0 % m/s | fdVXB: u 17 0 0 0 % m/s | fdVYB: v 18 0 0 0 % m/s | fdVZB: w 19 0 0 0 % m/s2 | fdVXED: vxedot acceleration 20 0 0 0 % m/s2 | fdVYED: vyedot acceleration 21 0 0 0 % m/s2 | fdVZED: vzedot acceleration 22 0 0 0 % m/s2 | fdVXBD: udot 23 0 0 0 24 0 0 0 25 0 0 0 % deg | fdROLL: Roll angle, phi 26 60 0 0 % deg | fdPITCH: Pitch angle, theta 27 0 0 0 % deg | fdYAW: Yaw angle, psi 28 0 0 0 % | fdE0: e0 quaternian 29 0 0 0 30 0 0 0 31 0 0 0 32 0 0 0 % deg/s| fdPE: pe angular velocity 33 0 0 0 34 0 0 0 35 0 0 0 % deg/s | fdROLLDOT: Roll angle rate, p (phi dot) 36 0 0 0 % deg/s | fdPITCHDOT: Pitch angle rate, q (theta dot) 37 0 0 0 % deg/s | fdYAWDOT: Yaw angle rate, r (psi dot) 38 0 0 0 % deg/s2 | fdPED: pedot angular acceleration 39 0 0 0 40 0 0 0 41 0 0 0 % deg/s2| fdROLLDOT2: Roll angle acceleration, pdot 42 0 0 0 % deg/s2| fdPITCHDOT2: Pitch angle acceleration, qdot 43 0 0 0 % deg/s2| fdYAWDOT2: Yaw angle acceleration, rdot %========================================================================================= % VEHICLE SECTION: %========================================================================================= %========================================================================================= % VEHICLE::PARAMETERS %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 45 55 2 5 % kg | vpMASS: Inert mass of the vehicle 46 1.0 2 .010 % m | vpLENGTH: Length 47 .275 2 .005 % m | vpDIA: Diameter %========================================================================================= % ENGINE SECTION: %========================================================================================= %========================================================================================= % ENGINE::GRAIN GEOMETRY %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 48 1.0 0 0 % in | egLP: Length of grain port 49 7.0 0 0 % -- | egNP: Number of ports 50 0.4 0 0 % in | egDP: Diameter of ports %========================================================================================= % ENGINE::NOZZLE %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 51 1.0 1 0.010 % in | enDT: Nozzle throat diameter 52 2.5 1 0.010 % in | enDE: Nozzle exit diameter 53 15.0 1 0.5 % deg | enLAMDA: Nozzle half angle 54 0.005 2 0.02 % in/s | enERATE: Nozzle throat errosion rate %========================================================================================= % ENGINE::OXIDIZER SYSTEM %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 55 0.053 1 0.002 % in | eoDIH: Diameter of injector holes 56 25 0 0 % -- | eoNIH: Number of injector holes 57 0.100 1 0.005 % in | eoLIH: Length of injector holes 58 0.8 2 0.2 % | eoCD: Coefficient of discharge for Ox System 59 1000 2 10 % psi | eoPOX: Oxidizer tank pressure 60 1100 2 50 % kg/m3 | eoROX: Oxidizer density 61 150 2 10 % K | eoTOX: Oxidizer temperature 62 10 2 2 % kg | eoMOX: Oxidizer mass %========================================================================================= % ENGINE::GRAIN CHEMISTRY %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 65 30 2 0.1 % kg | ecMFUEL: Mass of the fuel 66 2700 2 10.0 % g/mol | ecMWHTPB: Molecular weight of HTPB 67 222 2 1.0 % g/mol | ecMWIPDI: Molecular weight of IPDI 68 12 0 0 % g/mol | ecMWCARBON: Molecular weight of carbon black 69 0 0 0 % g/mol | ecMWCASTOR: Molecular weight of castor oil 70 901 0 0 % kg/m3 | ecRHTPB: Density of HTPB 71 1060 0 0 % kg/m3 | ecRIPDI: Density of IPDI 72 2267 0 0 % kg/m3 | ecRCARBON: Density of Carbon Black 73 962 0 0 % kg/m3 | ecRCASTOR: Density of Castor Oil 74 2 0 0 % -- | ecFHTPB: Functionality of HTPB 75 2 0 0 % -- | ecFIPDI: Functionality of IPDI 76 0 0 0 % -- | ecFCARBON: Functionality of carbon black 77 3 0 0 % -- | ecFCASTOR: Functionality of castor oil 78 1350 0 0 % g/mol | ecEWHTPB: Equivalent weight of HTPB 79 111 0 0 % g/mol | ecEWIPDI: Equivalent weight of IPDI 80 12 0 0 % g/mol | ecEWCARBON: Equivalent weight of carbon black 81 164 0 0 % g/mol | ecEWCASTOR: Equivalent weight of castor oil 82 0.0009 2 0.0001 % -- | ecMFCARBON: Mass fraction of carbon black 83 0.05 2 0.002 % -- | ecMFCASTOR: Mass fraction of castor oil %========================================================================================= % ENGINE::THERMOCHEMISTRY %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 85 800 0 0 %psi | etPC: Chamber pressure %========================================================================================= % ENVIRONMENT SECTION %========================================================================================= %========================================================================================= % ENVIRONMENT::WEATHER %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 90 293.0 1 20 % K | ewTAIR: Air temperature 91 101325 1 500 % Pa | ewPAIR: Air pressure 92 1.225 1 .2 % kg/m3 | ewRAIR: Air density 93 0 1 180 % deg | ewDWIND: Wind direction 94 10 1 10 % m/s | ewVWIND: Wind speed %========================================================================================= % ENVIRONMENT::MISC %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 96 9.81 0 0 % m/s2 | emGRAVITY: Gravity at the vehicle height 97 1.4005 0 0 % | emGAMMA: Coefficient of specific heat for air 98 287.1 0 0 % J/kg/K| emR: Gas constant for air %========================================================================================= % AERODYNAMICS SECTION %========================================================================================= %========================================================================================= % AERODYNAMICS::COEFFICIENTS %========================================================================================= %ARRAY| VALUE | MONTE | MC | units | NAME: DESC %LOC | | CARLO | SIGMA | | %========================================================================================= 105 0 0 0 % | acCD: Coefficient of drag 106 0 0 0 % | acFDX: Drag force in body x 107 0 0 0 % | acFDY: Drag force in body y 108 0 0 0 % | acFDZ: Drag force in body z 109 0 0 0 % | acMDX: Drag moment about body x 110 0 0 0 % | acMDY: Drag moment about body y 111 0 0 0 % | acMDZ: Drag moment about body z 112 0 0 0 % | acCL: Coefficient of lift 113 0 0 0 % | acFLX: Lift force in body x 114 0 0 0 % | acFLY: Lift force in body y 115 0 0 0 % | acFLZ: Lift force in body z 116 0 0 0 % | acMLX: Lift moment about body x 117 0 0 0 % | acMLY: Lift moment about body y 118 0 0 0 % | acMLZ: Lift moment about body z %========================================================================================= % CONTROL SYSTEM SECTION %=========================================================================================