WOLFRAM SYSTEM MODELER
VariableRotationIntroduce rotation of the blades of the propeller with respect to the motor |
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Wolfram Language
In[1]:=
SystemModel["Aircraft.Utilities.VariableRotation"]
Out[1]:=
Information
This component rotates frame_b according to the specified angle input and it connects to the frame_a which is the center of the propeller; and frame_b is connected to the propeller blade CAD shape.
Parameters (8)
| r |
Value: {0, 0, 0} Type: Position[3] (m) Description: Vector from frame_a to frame_b resolved in frame_a |
|---|---|
| n |
Value: {1, 0, 0} Type: Axis Description: Axis of rotation in frame_a (= same as in frame_b) |
| n_x |
Value: {1, 0, 0} Type: Axis Description: Vector along x-axis of frame_b resolved in frame_a |
| n_y |
Value: {0, 1, 0} Type: Axis Description: Vector along y-axis of frame_b resolved in frame_a |
| widthDirection |
Value: {0, 1, 0} Type: Axis Description: Vector in width direction of shape, resolved in frame_a |
| length |
Value: Modelica.Math.Vectors.length(r) Type: Length (m) Description: Length of shape |
| width |
Value: length / world.defaultWidthFraction Type: Distance (m) Description: Width of shape |
| height |
Value: width Type: Distance (m) Description: Height of shape. |
Connectors (3)
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frame_a |
Type: Frame_a Description: Coordinate system fixed to the component with one cut-force and cut-torque |
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frame_b |
Type: Frame_b Description: Coordinate system fixed to the component with one cut-force and cut-torque |
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angle |
Type: RealInput Description: Angle to rotate frame_a around axis n into frame_b |
Components (3)
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R_rel |
Type: Orientation Description: Orientation object defining rotation from a frame 1 into a frame 2 |
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world |
Type: World Description: World coordinate system + gravity field + default animation definition |
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R_rel_inv |
Type: Orientation Description: Inverse of R_rel (rotate from frame_b to frame_a) |
Used in Components (1)
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Aircraft.Physical.RotaryWing.MultiRotor.Parts.Propulsions Propeller of the quadrotor with two blades |