Parameters
Presets
Spin rate ω_spin
3000 RPM
Rotor mass m
0.50 kg
Rotor radius r
10.0 cm
Pivot distance d
10.0 cm
Tilt angle θ
90.0 °
90° = horizontal spin axis
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Angular momentum L [kg·m²/s]
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Gravitational torque τ [N·m]
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Precession rate Ω_p [rad/s]
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Nutation freq. [rad/s]
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Gyroscopic stiffness [N·m·s]
Precession rate vs Spin rate
Angular momentum vs Spin rate
Theory
Fundamental equations of angular momentum and precession:
$$\vec{\tau} = \frac{d\vec{L}}{dt}, \quad L = I\omega$$ $$I = \frac{1}{2}mr^2 \text{ (solid disk)}, \quad \omega = \frac{2\pi \cdot \text{RPM}}{60}$$ $$\Omega_p = \frac{\tau}{L\sin\theta} = \frac{mgd}{I\omega\sin\theta}$$Nutation frequency estimate: $\omega_n \approx \dfrac{L}{I_{trans}}$ (symmetric top approximation)
CAE applications: Spacecraft attitude control (reaction wheels, CMGs) / Rotating machinery Campbell diagram and bearing load analysis / Vehicle gyroscopic effects in suspension design / IMU sensor error evaluation in inertial navigation.