When I tried running the code to get the Aerodynamic coefficients, it gave me a message saying this:
"
Unrecognized field name "allmove".
Error in fLattice_setup2 (line 96)
if geo.allmove(tx)==0;
Error in computeAerodynamicCoefficients (line 171)
[lattice,ref]=fLattice_setup2(geo,state,lattictype);
Error in mainComputeCoefficients (line 63)
[alpha, beta, CX, CY, CZ, Cl, Cm, Cn, CX_d, CY_d, CZ_d, Cl_d, Cm_d, Cn_d, CX_P, CY_P, CZ_P, Cl_P, Cm_P, Cn_P, CX_Q, CY_Q, CZ_Q, Cl_Q, Cm_Q, Cn_Q, CX_R, CY_R, CZ_R, Cl_R, Cm_R, Cn_R]=computeAerodynamicCoefficients(aircraft_geometry_name, state, tornado_root_directory, alphaStart, alphaEnd, numAlphas, betaStart, betaEnd, numBetas, centerOfGravity);
"
I don't know why it can't read the geo.allmove thing
When I tried running the code to get the Aerodynamic coefficients, it gave me a message saying this:
"
Unrecognized field name "allmove".
Error in fLattice_setup2 (line 96)
if geo.allmove(tx)==0;
Error in computeAerodynamicCoefficients (line 171)
[lattice,ref]=fLattice_setup2(geo,state,lattictype);
Error in mainComputeCoefficients (line 63)
[alpha, beta, CX, CY, CZ, Cl, Cm, Cn, CX_d, CY_d, CZ_d, Cl_d, Cm_d, Cn_d, CX_P, CY_P, CZ_P, Cl_P, Cm_P, Cn_P, CX_Q, CY_Q, CZ_Q, Cl_Q, Cm_Q, Cn_Q, CX_R, CY_R, CZ_R, Cl_R, Cm_R, Cn_R]=computeAerodynamicCoefficients(aircraft_geometry_name, state, tornado_root_directory, alphaStart, alphaEnd, numAlphas, betaStart, betaEnd, numBetas, centerOfGravity);
"
I don't know why it can't read the geo.allmove thing