Starmac
Starmac is available as:
Simulation of the Stanford Testbed of Autonomous Quadrotor Aircraft
This model simulates the flight dynamics of the Starmac quadrotor aircraft
and then uses Java3D to show the results.
Vehicle Dynamics State:
- Ve - Velocity, earth fixed frame (what the velocity appears to be to an
outside observer, i.e., a vehicle heading North-East has its speed split
[in an norm sense] between the x and y components)
- Ab - Acceleration.
- Xe - Position, earth fixed frame.
- p,q,r - Angular velocity, body fixed frame.
- DCM - Direction cosine matrix, a.k.a. rotation matrix. Rotates a vector
between the body frame and the earth fixed frame.
- Euler - The Euler angles.