A nonlinear dynamics theory is presented for modeling air bearing slider sy
stems. The nonlinear dynamic coefficients are acquired by fitting the datab
ase of the discrete linear dynamic coefficients. The linear dynamic coeffic
ients for an air bearing slider around steady flying state are calculated b
y using a Reynolds-equation-based perturbation method. A nonlinear analysis
shows that the natural frequencies of the system decrease with the increas
e of slider vibration amplitude, and that the softening feature of the syst
em bends the resonance to lower frequency and complicates the system vibrat
ions. The analysis correlates with experimental results. (C) 2000 American
Institute of Physics. [S0021- 8979(00)84508-9].