Closed fguecker closed 1 year ago
After updating the state equations block, the parameter mass and inertia matrix have been overwritten with default values. The values are fixed to the proper values from the airplane.body struct as following:
1) mass: 1 -> airplane.body.m
2) inertia matrix: eye(3) -> airplane.body.I
After updating the state equations block, the parameter mass and inertia matrix have been overwritten with default values. The values are fixed to the proper values from the airplane.body struct as following:
1) mass: 1 -> airplane.body.m
2) inertia matrix: eye(3) -> airplane.body.I