Tez Dosyaları 4
Aerodynamic parameter estimation of a supersonic missile with rapid speed variation by using kalman filtering
Kill analysis tool for missiles equipped with proximity fuzes
Development of a high-fidelity transient aerothermal model for a helicopter turboshaft engine for inlet distortion and engine deterioration simulations
Stochastic and deterministic analysis of nonlinear of nonlinear missile engagement scenarios using 5-dof 6-dof and adjoint model