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REL: v1.1.4 #503

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17 changes: 13 additions & 4 deletions CHANGELOG.md
Original file line number Diff line number Diff line change
Expand Up @@ -42,14 +42,23 @@ straightforward as possible.

-

## [v1.1.3] - 2023-11-29
## [v1.1.4] - 2023-12-07

Here we write upgrading notes for brands. It's a team effort to make them as
straightforward as possible.
You can install this version by running `pip install rocketpy==1.1.4`

### Fixed

- DOC: Change from % to ! in the first cell to run properly in Colab. [#496](https://github.com/RocketPy-Team/RocketPy/pull/496)
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This line is not necessary for changelog. I'm going to update the changelog description to avoid future mistakes.

PLease don't accept suggestion

Suggested change
- DOC: Change from % to ! in the first cell to run properly in Colab. [#496](https://github.com/RocketPy-Team/RocketPy/pull/496)

- FIX: changes Generic Motor exhaust velocity to cached property [#497](https://github.com/RocketPy-Team/RocketPy/pull/497)

## [v1.1.3] - 2023-11-30

You can install this version by running `pip install rocketpy==1.1.3`

### Fixed

- FIX: Broken Function.get_value_opt for N-Dimensional Functions [#492](https://github.com/RocketPy-Team/RocketPy/pull/492/files)
- FIX: Broken Function.get_value_opt for N-Dimensional Functions [#492](https://github.com/RocketPy-Team/RocketPy/pull/492)
- FIX: Never ending Flight simulations when using a GenericMotor [#497](https://github.com/RocketPy-Team/RocketPy/pull/497)

## [v1.1.2] - 2023-11-25

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2 changes: 1 addition & 1 deletion docs/conf.py
Original file line number Diff line number Diff line change
Expand Up @@ -24,7 +24,7 @@
author = "RocketPy Team"

# The full version, including alpha/beta/rc tags
release = "1.1.3"
release = "1.1.4"


# -- General configuration ---------------------------------------------------
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4 changes: 2 additions & 2 deletions docs/notebooks/deployable_payload_example.ipynb
Original file line number Diff line number Diff line change
Expand Up @@ -44,8 +44,8 @@
"metadata": {},
"outputs": [],
"source": [
"%pip install rocketpy netCDF4\n",
"%git clone https://github.com/RocketPy-Team/RocketPy.git"
"!pip install rocketpy netCDF4\n",
"!git clone https://github.com/RocketPy-Team/RocketPy.git"
]
},
{
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Original file line number Diff line number Diff line change
Expand Up @@ -37,7 +37,7 @@
"metadata": {},
"outputs": [],
"source": [
"%git clone https://github.com/RocketPy-Team/RocketPy.git\n",
"!git clone https://github.com/RocketPy-Team/RocketPy.git\n",
"import os\n",
"\n",
"os.chdir(\"RocketPy/docs/notebooks/dispersion_analysis\")"
Expand Down Expand Up @@ -66,8 +66,7 @@
},
"outputs": [],
"source": [
"%pip install netCDF4\n",
"%pip install rocketpy"
"!pip install rocketpy"
]
},
{
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Original file line number Diff line number Diff line change
Expand Up @@ -31,7 +31,7 @@
"metadata": {},
"outputs": [],
"source": [
"%git clone https://github.com/giovaniceotto/RocketPy.git\n",
"!git clone https://github.com/giovaniceotto/RocketPy.git\n",
"import os\n",
"\n",
"os.chdir(\"RocketPy/docs/notebooks/dispersion_analysis\")"
Expand Down Expand Up @@ -60,8 +60,7 @@
},
"outputs": [],
"source": [
"%pip install netCDF4\n",
"%pip install rocketpy"
"!pip install rocketpy"
]
},
{
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19 changes: 4 additions & 15 deletions docs/notebooks/getting_started_colab.ipynb
Original file line number Diff line number Diff line change
Expand Up @@ -22,10 +22,9 @@
"We start by setting up our environment. To run this notebook, we will need:\n",
"\n",
"- RocketPy\n",
"- netCDF4 (to get weather forecasts)\n",
"- Data files (we will clone RocketPy's repository for these)\n",
"\n",
"Therefore, let's run the following lines of code:\n"
"Therefore, let's run the following lines of code:"
]
},
{
Expand All @@ -38,8 +37,8 @@
},
"outputs": [],
"source": [
"%pip install rocketpy netCDF4\n",
"%git clone https://github.com/giovaniceotto/RocketPy.git"
"!pip install rocketpy\n",
"!git clone https://github.com/giovaniceotto/RocketPy.git"
]
},
{
Expand Down Expand Up @@ -70,16 +69,6 @@
"Here we go through a simplified rocket trajectory simulation to get you started. Let's start by importing the rocketpy module.\n"
]
},
{
"cell_type": "code",
"execution_count": null,
"metadata": {},
"outputs": [],
"source": [
"%load_ext autoreload\n",
"%autoreload 2"
]
},
{
"cell_type": "code",
"execution_count": 1,
Expand All @@ -101,7 +90,7 @@
"id": "ImgkhEkZNVE8"
},
"source": [
"If you are using Jupyter Notebooks, it is recommended to run the following line to make matplotlib plots which will be shown later interactive and higher quality.\n"
"It is recommended to run the following line to make matplotlib plots which will be shown later interactive and higher quality.\n"
]
},
{
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2 changes: 1 addition & 1 deletion docs/user/installation.rst
Original file line number Diff line number Diff line change
Expand Up @@ -19,7 +19,7 @@ If you want to choose a specific version to guarantee compatibility, you may ins

.. code-block:: shell

pip install rocketpy==1.1.3
pip install rocketpy==1.1.4


Optional Installation Method: ``conda``
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6 changes: 4 additions & 2 deletions rocketpy/motors/hybrid_motor.py
Original file line number Diff line number Diff line change
@@ -1,4 +1,4 @@
from ..mathutils.function import funcify_method, reset_funcified_methods
from ..mathutils.function import Function, funcify_method, reset_funcified_methods
from ..plots.hybrid_motor_plots import _HybridMotorPlots
from ..prints.hybrid_motor_prints import _HybridMotorPrints
from .liquid_motor import LiquidMotor
Expand Down Expand Up @@ -372,7 +372,9 @@ def exhaust_velocity(self):
self.exhaust_velocity : Function
Gas exhaust velocity of the motor.
"""
return self.total_impulse / self.propellant_initial_mass
return Function(
self.total_impulse / self.propellant_initial_mass
).set_discrete_based_on_model(self.thrust)

@funcify_method("Time (s)", "Mass (kg)")
def propellant_mass(self):
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4 changes: 3 additions & 1 deletion rocketpy/motors/motor.py
Original file line number Diff line number Diff line change
Expand Up @@ -1224,7 +1224,9 @@ def exhaust_velocity(self):
self.exhaust_velocity : Function
Gas exhaust velocity of the motor.
"""
return self.total_impulse / self.propellant_initial_mass
return Function(
self.total_impulse / self.propellant_initial_mass
).set_discrete_based_on_model(self.thrust)

@funcify_method("Time (s)", "Mass Flow Rate (kg/s)")
def mass_flow_rate(self):
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4 changes: 3 additions & 1 deletion rocketpy/motors/solid_motor.py
Original file line number Diff line number Diff line change
Expand Up @@ -381,7 +381,9 @@ def exhaust_velocity(self):
self.exhaust_velocity : Function
Gas exhaust velocity of the motor.
"""
return self.total_impulse / self.propellant_initial_mass
return Function(
self.total_impulse / self.propellant_initial_mass
).set_discrete_based_on_model(self.thrust)

@property
def propellant_initial_mass(self):
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2 changes: 1 addition & 1 deletion setup.py
Original file line number Diff line number Diff line change
Expand Up @@ -23,7 +23,7 @@

setuptools.setup(
name="rocketpy",
version="1.1.3",
version="1.1.4",
install_requires=necessary_require,
extras_require={
"env_analysis": env_analysis_require,
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