For the vehicle in Example 13.4.4, investigate the sensitivity of the bounce and pitch node location to uncertainty in the parameter values.
Rearrange the mode ratio expression to obtain
\frac{A_1}{A_2}=\frac{x}{\theta}=\frac{k_1 L_1 – k_2 L_2}{m} \frac{1}{\omega_1^2 – \omega^2}where we have defined ω² = −s², and ω_1 as the natural frequency of a concentrated mass m attached to two springs k_1 and k_2:
\omega_1=\sqrt{\frac{k_1 + k_2}{m}}The value of ω² = −s² is obtained from the characteristic equation. If ω² is close to ω^2_1, then the denominator of x/θ will be very small, and x/θ will be very large. In addition, any slight change in the values of ω^2_1 or ω² due to changes in the parameters k_1, k_2, L_1, L_2, m, or I_G will cause large changes in the value of x/θ and thus large changes in the node location. In Example 13.4.4, ω^2_1 = 4.1 × 10^4/730 = 56.16. One of the roots gives s² = −57.61, which is close to −56.16. Thus we can expect large changes in the node location if slightly different parameter values are used. The other root gives s² = −47.63, which is not as close to −56.16; thus, the corresponding node location will not be as sensitive.
If it is important to have a reliable prediction for the node location, the parameters must be selected—usually by trial and error—so that ω² is not close to ω^2_1.