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6 changes: 6 additions & 0 deletions rocketpy/Flight.py
Original file line number Diff line number Diff line change
Expand Up @@ -62,6 +62,8 @@ class Flight:
Original rail length minus the distance measured from nozzle exit
to the lower rail button. It assumes the nozzle to be aligned with
the beginning of the rail.
Flight.name: str
Name of the flight.


Numerical Integration settings:
Expand Down Expand Up @@ -527,6 +529,7 @@ def __init__(
atol=6 * [1e-3] + 4 * [1e-6] + 3 * [1e-3],
timeOvershoot=True,
verbose=False,
name="Flight",
):
"""Run a trajectory simulation.

Expand Down Expand Up @@ -582,6 +585,8 @@ def __init__(
time in some cases. Default is True.
verbose : bool, optional
If true, verbose mode is activated. Default is False.
name : str, optional
Name of the flight. Default is "".
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Returns
-------
Expand All @@ -607,6 +612,7 @@ def __init__(
self.initialSolution = initialSolution
self.timeOvershoot = timeOvershoot
self.terminateOnApogee = terminateOnApogee
self.name = name

# Modifying Rail Length for a better out of rail condition
upperRButton = max(self.rocket.railButtons[0])
Expand Down