Aviary
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OpenMDAO
NASA's aircraft analysis, design, and optimization tool
### Desired capability or behavior. 1. Move the throttle balance solver loop in missionODE into its own subsystem. 2. Allow any external subsystem builder to specify whether it should be...
### Description Right now, we promote `aircraft:*` and `mission:*` out of any external subsystem that is added to the mission. We discovered that we are missing promotion of state variables,...
### Desired capability or behavior. Currently, EOMs in Aviary do not use a consistent way to define forces and motion. A ground-fixed axis to define forces and motion could be...
### Summary Follow on to #397 ### Related Issues - Resolves # ### Backwards incompatibilities None ### New Dependencies None
### Description The Optimization -> History plot in the dashboard has formatting and usability issues. 1. No units on the X axes 2. Legend is not in an optimum location...
### Desired capability or behavior. Currently, Aviary generates an N2 model after model setup. It is very helpful to have this "early" N2 in case you need to debug a...
### Desired capability or behavior. The naming for non-sizing mission types are inherited from GASP ("fallout" and "alternate"). These names are not very descriptive (their purpose cannot be guessed from...
### Desired capability or behavior. Every time testflo is run, a very large number of reports are generated, but in general are unneeded. Report generation should be suppressed, either through...
### Desired capability or behavior. In examples and documentation, we frequently make use of the IPOPT and SNOPT optimizers. We need to make sure all introductory documentation examples and in-source-code...
### Desired capability or behavior. Add option to create detailed landing phase using build_takeoff.py ### Is your feature request related to a problem? Please describe. _No response_ ### Associated Bug...