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BUG: Cld divided by zero
- #122
#122
Merged
MateusStano
merged 12 commits into
RocketPy-Team:develop
RocketPy-Team/RocketPy:develop
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MateusStano:bug/Cld-diveded-by-zero
MateusStano/RocketPy:bug/Cld-diveded-by-zero
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Feb 12, 2022
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BUG: Cld divided by zero
#122
MateusStano
merged 12 commits into
RocketPy-Team:develop
RocketPy-Team/RocketPy:develop
from
MateusStano:bug/Cld-diveded-by-zero
MateusStano/RocketPy:bug/Cld-diveded-by-zero
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Commits
Commits on Jan 11, 2022
Changed the solution to division by zero to a more trustful one
MateusStano
committed
977f7e1
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Commits on Feb 6, 2022
Fixed lift coefficient, roll coefficients and roll moment calculations
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d941e6e
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ran black and pytest
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db8531b
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Removed unnecessary Function() on cldOmega
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Commits on Feb 10, 2022
MAINT: change aerodynamic surfaces to dictionaries
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MAINT: change aerodynamic surfaces to dictionaries
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Added/Fixed suggested changes
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920f653
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Added pytest for rolling flight
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Commits on Feb 12, 2022
Reformated M3d equation.
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Merge branch 'develop' into bug/Cld-diveded-by-zero
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Removed cantAngleRad != 0 check on rollParameters
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Merge branch 'bug/Cld-diveded-by-zero' of https://github.com/MateusStano/RocketPy into bug/Cld-diveded-by-zero
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