feat: Shoulder joint follow wing direction
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@ -63,6 +63,7 @@ class ShoulderJoint(Model):
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axis_rotate_top: float = -225.0
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axis_rotate_top: float = -225.0
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directrix_id: int = 0
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directrix_id: int = 0
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angle_neutral: float = 10.0
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def __post_init__(self):
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def __post_init__(self):
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assert self.parent_lip_length * 2 < self.height
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assert self.parent_lip_length * 2 < self.height
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@ -189,8 +190,8 @@ class ShoulderJoint(Model):
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)
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)
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theta = self.torsion_joint.spring.angle_neutral - self.torsion_joint.rider_slot_span
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theta = self.torsion_joint.spring.angle_neutral - self.torsion_joint.rider_slot_span
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loc_rotate = Cq.Location((0, 0, 0), (1, 0, 0), 180)
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loc_rotate = Cq.Location((0, 0, 0), (1, 0, 0), 180)
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loc_axis_rotate_bot = Cq.Location((0, 0, 0), (0, 0, 1), self.axis_rotate_bot)
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loc_axis_rotate_bot = Cq.Location((0, 0, 0), (0, 0, 1), self.axis_rotate_bot + self.angle_neutral)
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loc_axis_rotate_top = Cq.Location((0, 0, 0), (0, 0, 1), self.axis_rotate_top)
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loc_axis_rotate_top = Cq.Location((0, 0, 0), (0, 0, 1), self.axis_rotate_top + self.angle_neutral)
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result = (
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result = (
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Cq.Assembly()
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Cq.Assembly()
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.add(core, name="core", loc=Cq.Location())
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.add(core, name="core", loc=Cq.Location())
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@ -93,6 +93,8 @@ class WingProfile(Model):
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self.wrist_s = math.sin(self.wrist_theta)
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self.wrist_s = math.sin(self.wrist_theta)
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self.wrist_top_x, self.wrist_top_y = self.wrist_to_abs(0, self.wrist_height)
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self.wrist_top_x, self.wrist_top_y = self.wrist_to_abs(0, self.wrist_height)
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self.shoulder_joint.angle_neutral = -self.shoulder_angle_neutral
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@submodel(name="shoulder-joint")
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@submodel(name="shoulder-joint")
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def submodel_shoulder_joint(self) -> Model:
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def submodel_shoulder_joint(self) -> Model:
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return self.shoulder_joint
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return self.shoulder_joint
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@ -180,6 +182,17 @@ class WingProfile(Model):
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#)
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#)
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)
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)
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@property
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def shoulder_angle_neutral(self) -> float:
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"""
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Returns the neutral angle of the shoulder
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"""
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dx = self.shoulder_mid_x - self.shoulder_tip_x
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dy = -(self.shoulder_mid_y - (self.shoulder_tip_y - self.shoulder_width))
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result = math.degrees(math.atan2(dy, dx))
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assert result >= 0
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return result
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@target(name="profile-s0", kind=TargetKind.DXF)
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@target(name="profile-s0", kind=TargetKind.DXF)
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def profile_s0(self) -> Cq.Sketch:
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def profile_s0(self) -> Cq.Sketch:
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tip_x = self.shoulder_tip_x
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tip_x = self.shoulder_tip_x
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@ -270,10 +283,17 @@ class WingProfile(Model):
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def surface_s0(self, top: bool = False) -> Cq.Workplane:
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def surface_s0(self, top: bool = False) -> Cq.Workplane:
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base_dx = -(self.base_width - self.base_plate_width) / 2
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base_dx = -(self.base_width - self.base_plate_width) / 2
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base_dy = self.base_joint.joint_height
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base_dy = self.base_joint.joint_height
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sw = self.shoulder_width
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axle_dist = self.shoulder_joint.parent_lip_ext
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axle_dist = self.shoulder_joint.parent_lip_ext
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theta = math.radians(self.shoulder_joint.angle_neutral)
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c, s = math.cos(-theta), math.sin(-theta)
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tags = [
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tags = [
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("shoulder", (self.shoulder_tip_x + axle_dist, self.shoulder_tip_y - self.shoulder_width), 0),
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# transforms [axle_dist, -sw/2] about the centre (tip_x, tip_y - sw/2)
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("shoulder", (
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self.shoulder_tip_x + axle_dist * c + (-sw/2) * s,
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self.shoulder_tip_y - sw / 2 - axle_dist * s + (-sw/2) * c),
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self.shoulder_joint.angle_neutral),
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("base", (base_dx, base_dy), 90),
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("base", (base_dx, base_dy), 90),
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]
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]
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result = nhf.utils.extrude_with_markers(
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result = nhf.utils.extrude_with_markers(
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