Chris Bennett

@Kenneth-T-Moore and I discussed this in detail, and we think that this issue could be closed with no change. The initial guesses specified in phase info are all treated as...

Update - Thanks @kaushikponnapalli & @crecine for the help. Sometimes Mass is used as the integration variable (2DOF, Cruise), and so we need to be able to handle this case....

I created this issue as it was something Carl, Kaushik and I found whilst doing some other testing/development. We just ran the test_bench_GwGm.py file with the above command "python test_bench_GwGm.py"...

I think FLOPS also has a fighter/attack aircraft option (IFITE = 1) Are we planning to include this functionality in Aviary? 

This would address the 'TODO' in line 2558 of variable_meta_data.py: 

 Fuel Density also seems to swap between being specified as lbm/usgal and lbm/ft**3 within the fuel.py script for GASP based missions. This should be corrected for consistency. picture is...

Aircraft.Fuel.TOTAL_VOLUME is not currently calculated in Aviary as it has been commented out of the unusable fuel component. In the same way as Aviary should calculate the 3rd of Span,...

FwFm benchmark with IPOPT comparison of command Line Output from main branch (left) and des_var_bounds branch with upper bounds set = None:  It seems that there is no difference...

GwGm benchmark with IPOPT comparison of Command Line Output from the main branch (left) and the des_var_bounds branch with upper_bounds set = None:  Difference in number of variables with...

@Kenneth-T-Moore - I've Run FwFm and GwGm, which I think covers Height Energy and Two Degrees of Freedom mission methods - do we have a SOLVED_2DOF benchmark too, I see...