### Install MachUpX

Source: https://machupx.readthedocs.io/en/latest/_sources/installation.md.txt

Install the package from the root directory.

```bash
$ pip install .
```

--------------------------------

### Verify Installation

Source: https://machupx.readthedocs.io/en/latest/_sources/installation.md.txt

Run tests to ensure the installation is functioning correctly.

```bash
$ py.test
```

```bash
> py.test-script.py
```

--------------------------------

### Install FreeCAD on Linux

Source: https://machupx.readthedocs.io/en/latest/_sources/installation.md.txt

Install FreeCAD using the apt package manager.

```bash
$ sudo apt-get install freecad
```

--------------------------------

### Check Git Version

Source: https://machupx.readthedocs.io/en/latest/_sources/installation.md.txt

Verify if Git is installed on your system.

```bash
git --version
```

--------------------------------

### Define Scene Run Commands

Source: https://machupx.readthedocs.io/en/latest/_sources/creating_input_files.md.txt

Example of configuring the 'run' dictionary within a scene JSON object to execute trim, force solving, and derivative calculations.

```json
{
    ...
    "run" : {
        "pitch_trim" : {
            "set_trim_state" : true,
            "verbose" : true
        },
        "solve_forces" : {
            "filename" : "my_forces.json",
            "dimensional" : false,
            "nondimensional" : false,
            "verbose" : true
        },
        "derivatives" : {
            "filename" : "my_derivatives.json"
        }
    },
    ...
}
```

--------------------------------

### Define Custom Spanwise Distribution

Source: https://machupx.readthedocs.io/en/latest/_sources/creating_input_files.md.txt

Example format for providing an explicit list of span locations for vortex nodes and control points.

```json
[node_0_loc, cp_0_loc, node_1_loc, cp_1_loc,..., node_N_loc, cp_N_loc, node_N+1_loc]
```

--------------------------------

### Interact with MachUpX via Python Interpreter

Source: https://machupx.readthedocs.io/en/latest/_sources/user_interface.md.txt

Demonstrates initializing a scene, displaying wireframes, solving forces, trimming, and calculating derivatives using the Scene class.

```python
import machupX as MX

input_file = "traditional_input.json"

# Initialize scene
my_scene = MX.Scene(input_file)

# Display wireframe of the scene
my_scene.display_wireframe(show_legend=True)

# Solve aerodynamic forces and moments
FM_results = my_scene.solve_forces(dimensional=True, non_dimensional=False, verbose=True)
print(json.dumps(FM_results["traditional_airplane"]["total"], indent=4))

# Trim the aircraft in pitch
trim_state = my_scene.aircraft_pitch_trim(set_trim_state=True, verbose=True)
print(json.dumps(trim_state["traditional_airplane"]))

# Calculate aerodynamic derivatives
derivs = my_scene.aerodynamic_derivatives()
print(json.dumps(derivs["traditional_plane"]))
```

--------------------------------

### Clone MachUpX Repository

Source: https://machupx.readthedocs.io/en/latest/_sources/installation.md.txt

Download the source code from the official GitHub repository.

```bash
$ git clone https://github.com/usuaero/MachUpX
```

--------------------------------

### Run MachUpX via Command Line

Source: https://machupx.readthedocs.io/en/latest/_sources/user_interface.md.txt

Executes analysis defined in a JSON input file using the MachUpX module.

```python
python -m machupX example_input.json
```

--------------------------------

### Configure FreeCAD Python Path

Source: https://machupx.readthedocs.io/en/latest/_sources/installation.md.txt

Add FreeCAD modules to the Python path using conda-develop.

```bash
$ conda-develop /usr/lib/freecad/lib
$ conda-develop /usr/lib/freecad/bin
$ conda-develop /usr/lib/freecad/bin/lib
$ conda-develop /usr/lib/freecad/Ext
$ conda-develop /usr/lib/freecad/Mod
$ conda-develop /usr/lib/freecad/Gui
```

--------------------------------

### Update MachUpX Repository

Source: https://machupx.readthedocs.io/en/latest/_sources/installation.md.txt

Pull the latest changes from the repository.

```bash
$ git pull
```

--------------------------------

### Debugging DatabaseBoundsError

Source: https://machupx.readthedocs.io/en/latest/_sources/common_issues.md.txt

Use a try-except block to catch DatabaseBoundsError and inspect the specific airfoil, indices, and input parameters causing the interpolation failure.

```python
try:
    scene.solve_forces()
except airfoil_db.DatabaseBoundsError as e:
    print(e.airfoil)
    print(e.exception_indices)
    print(e.inputs_dict)
```

--------------------------------

### Define a Step Change in Twist Distribution

Source: https://machupx.readthedocs.io/en/latest/_sources/creating_input_files.md.txt

Use an array of span fractions and twist values to create a step change in the wing twist distribution.

```json
"twist" : [[0.0, 0.0], [0.5, 0.0], [0.5, 2.0], [1.0, 2.0]]
```

--------------------------------

### Scene.set_err_state()

Source: https://machupx.readthedocs.io/en/latest/_sources/error_handling.rst.txt

Configures how errors are processed within the MachUpX environment, allowing them to be treated as warnings or suppressed entirely.

```APIDOC
## Scene.set_err_state()

### Description
Sets the global error handling state for the MachUpX scene. This allows users to toggle between raising errors, logging them as warnings, or suppressing them.

### Usage
`Scene.set_err_state(state)`
```

--------------------------------

### Custom Error Classes

Source: https://machupx.readthedocs.io/en/latest/_sources/error_handling.rst.txt

Overview of the custom error exceptions that may be raised during MachUpX operations.

```APIDOC
## Custom Error Classes

### SolverNotConvergedError
Raised when the numerical solver fails to reach a converged state.

### DatabaseBoundsError
Raised when input parameters fall outside the defined bounds of the airfoil database. Note: Angular values such as 'alpha' and 'trailing_flap_deflection' are reported in radians.
```

--------------------------------

### Calculate Aerodynamic Center (Phillips' Approximation)

Source: https://machupx.readthedocs.io/en/latest/_sources/developer_notes.md.txt

General formula for the aerodynamic center using Phillips' approximation.

```text
                    /     b/2            \
    _      1    d  |     /       ~       |
    x   = ----  -- |     |  CL c x   dy  |
     ac   CL,a  da |     /        ac     |
                    \-b/2               /
```

--------------------------------

### Define an Elliptic Chord Distribution

Source: https://machupx.readthedocs.io/en/latest/_sources/creating_input_files.md.txt

Specify an elliptic chord distribution by providing the root chord length and optional units.

```json
"chord" : ["elliptic", 1.0]
```

```json
"chord" : ["elliptic", 1.0, "ft"]
```

--------------------------------

### Calculate Aerodynamic Center (Constant Section Lift Coefficient)

Source: https://machupx.readthedocs.io/en/latest/_sources/developer_notes.md.txt

Simplified formula for the aerodynamic center assuming constant section lift coefficient over the span.

```text
                b/2
    _     1    /     ~
    x   = -    |   c x   dy
     ac   S    /      ac
           -b/2
```

--------------------------------

### Specify column units in CSV files

Source: https://machupx.readthedocs.io/en/latest/_sources/units.md.txt

Add a final row to a CSV file to define the units for each column.

```csv
# File: density_profile.csv
0.0, 1.225
2000.0, 1.0066
4000.0, 0.81935
"m", "kg/m^3"
```

--------------------------------

### Specify units for float values

Source: https://machupx.readthedocs.io/en/latest/_sources/units.md.txt

Define units for a single float value by providing a list containing the value and the unit string.

```json
"area" : [6.75, "ft^2"]
```

--------------------------------

### Calculate Mean Aerodynamic Chord (MAC)

Source: https://machupx.readthedocs.io/en/latest/developer_notes.html

Mathematical definition of the Mean Aerodynamic Chord as a reference length based on Phillips Eq. 1.8.86.

```text
            b/2
      1    /     2
MAC = -    |    c  dy
      S    /
       -b/2
```

--------------------------------

### Specify units for vector inputs

Source: https://machupx.readthedocs.io/en/latest/_sources/units.md.txt

Append the unit string as the final element in a vector input.

```json
"velocity" : [100.0, 13.0, 0.0, "ft/s"]
```

--------------------------------

### Specify units for array inputs

Source: https://machupx.readthedocs.io/en/latest/_sources/units.md.txt

Include units as an additional row at the end of an array structure.

```json
"rho" : [[0.0, 1.225],
         [2000.0, 1.0066],
         [4000.0, 0.81935],
         ["m", "kg/m^3"]]
```

--------------------------------

### Identify Trailing Vortex Impingement Warning

Source: https://machupx.readthedocs.io/en/latest/common_issues.html

This warning indicates that a control point is too close to a trailing vortex, which can be suppressed by adjusting the impingement_threshold in the solver parameters.

```text
MachUpX detected a trailing vortex impinging upon a control point. This can lead to greatly exaggerated induced velocities at the control point.
See "Common Issues" in the documentation for more information. This warning can be suppressed by reducing "impingement_threshold" in the solver parameters.
```

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