Global Aircraft Dynamics Using Piecewise Volterra Kernels

摘要: Evaluating global aircraft dynamic behavior by Volterra theory as an efficient nonlinear approximation method is investigated. In previous research, implemented to evaluate the system in a selected local region of state space, which restricts ability capture while moving from one flight another. The current research presents piecewise kernel approach. approach utilizes sub-model kernels build kernels. A novel strength index proposed determine number required terms each sub-model. interpolation then employed switch between sub-models. An approximate pitch-plunge model for F-18 was used assess set experimental simulations conducted verify capability capturing aircraft. compared with linear employing simulation benchmark.