# Enter a name for your vehicle
vehicle_name: plane_example_2

# Enter the type of airframe you would like to use:
frame_type: custom

# First define some model-wide parameters for custom models:
reference_area: 12
wing_span: 15
# Provide a reference point at which the forces and moments generated will act.
reference_point:
  X: 0
  Y: 0
  Z: 0

#Provide information on each of the Control Surfaces
num_ctrl_surfaces: 4
control_surfaces:
  - name: right_wing
    type: aileron
    nchord: 1
    cspace: 1
    nspan: 16
    sspace: -2
    angle: 4
    translation:
      X: 0
      Y: 0
      Z: 0
    naca: 2412
    sections:
    - name: section_1
      position:
        X: -0.25
        Y: 0
        Z: 0
      chord: 1
      ainc: 0
      nspan: 8
      sspace: 1
    - name: section_2
      position:
        X: -0.175
        Y: 5
        Z: 0.5
      chord: 0.7
      ainc: 0
      nspan: 0
      sspace: 0


  - name: left_wing
    type: aileron
    nchord: 1
    cspace: 1
    nspan: 16
    sspace: -2
    angle: 4
    translation:
      X: 0
      Y: 0
      Z: 0
    naca: 2412
    sections:
    - name: section_1
      position:
        X: -0.175
        Y: -5
        Z: 0.5
      chord: 0.7
      ainc: 0
      nspan: 0
      sspace: 0
    - name: section_2
      position:
        X: -0.25
        Y: 0
        Z: 0
      chord: 1
      ainc: 0
      nspan: 8
      sspace: 1

  - name: elevator
    type: elevator
    nchord: 1
    cspace: 1
    nspan: 7
    sspace: -2
    translation:
      X: 6
      Y: 0
      Z: 0.5
    sections:
    - name: section_1
      position:
        X: -0.1
        Y: 0
        Z: 0
      chord: 0.4
      ainc: 0
      nspan: 7
      sspace: -1.25
    - name: section_2
      position:
        X: -0.075
        Y: 2
        Z: 0
      chord: 0.3
      ainc: 0
      nspan: 0
      sspace: 0

  - name: fin
    type: rudder
    nchord: 1
    cspace: 1
    nspan: 10
    sspace: 1
    translation:
      X: 6
      Y: 0
      Z: 0.5
    sections:
    - name: section_1
      position:
        X: -0.1
        Y: 0
        Z: 0
      chord: 0.4
      ainc: 0
      nspan: 7
      sspace: -1.25
    - name: section_2
      position:
        X: -0.075
        Y: 0
        Z: 1
      chord: 0.3
      ainc: 0
      nspan: 0
      sspace: 0