Aviary

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### Desired capability or behavior. Add option to create detailed landing phase using build_landing.py ### Is your feature request related to a problem? Please describe. _No response_ ### Associated Bug...

jkirk5

### Desired capability or behavior. `mission/gasp_based/polynomial_fit.py` does not have analytic derivatives defined ### Is your feature request related to a problem? Please describe. _No response_ ### Associated Bug Report _No...

jkirk5

### Description Partials check fails for this component ### Example Change line 111 of `test_unsteady_solved_ode.py` to a reasonable tolerance: assert_check_partials(cpd, atol=1e-6, rtol=1e-6) ### Aviary Version 0.9.4-dev ### Relevant environment information...

jkirk5

### Description `mission/gasp_based/ode/unsteady_solved/test/test_unsteady_alpha_thrust_iter_group.py` and `mission/gasp_based/ode/unsteady_solved/test/test_unsteady_solved_ode.py` fail when `ground_roll=True` is enabled ### Example test = TestUnsteadyAlphaThrustIterGroup() self._test_unsteady_alpha_thrust_iter_group(ground_roll=True) ### Aviary Version 0.9.4-dev ### Relevant environment information _No response_

jkirk5

### Desired capability or behavior. Currently engines are responsible for providing analysis to determine what their maximum possible thrust output for a given flight condition is, for the purpose of...

jkirk5