- Added compatibility with OpenMDAO 3.2. - Added the mission performance module (currently computes a fixed standard mission). - Propulsion models are now declared in a specific way so that another module can do a direct call to the needed propulsion model.
0.4.2beta
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- Prevents installation of OpenMDAO 3.2 and above for incompatibility reasons. - In Breguet module, output values for climb and descent distances were 1000 times too large (computation was correct, though).
0.4.0beta
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Some changes in mass and performances components: - The Breguet performance model can now be adjusted through input variables in the "settings" section. - The mass-performance loop is now done through the "fastoad.loop.mtow" component.
0.3.1beta
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- Adapted the FAST-OAD code to handle OpenMDAO version 3.1.1.
0.3.0beta
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- In Jupyter notebooks, VariableViewer now has a column for input/output type. - Changed base OAD process so that propulsion model can now be directly called by the performance module instead of being a separate OpenMDAO component (which is still possible, though). It prepares the import of FAST legacy mission-based performance model.
0.2.2beta
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- Changed dependency requirement to have OpenMDAO version at most 3.1.0 (FAST-OAD is not yet compatible with 3.1.1)