Symbol | Definition | Value | Unit |
| Moment of inertia (pitch direction) | 0.0384 |
|
| Moment of inertia (yaw direction) | 0.0432 |
|
| Mass of the helicopter | 1.3872 |
|
| Distance from center of mass to yaw axis | 0.186 |
|
| Thrust torque constant acting on pitch axis from pitch motor | 0.204 |
|
| Thrust torque constant acting on yaw axis from yaw motor | 0.072 |
|
| Thrust torque constant acting on pitch axis from yaw motor | 0.0068 |
|
| Thrust torque constant acting on yaw axis from pitch motor | 0.0219 |
|
| Power voltage acting on the pitch motor | Variable |
|
| Power voltage acting on the yaw motor | Variable |
|