Simplified 3-Dimensional Surface-to-air Missile Model.

摘要

This thesis describes the development of a simplified 3-dimensional SAM model, a model that has been developed in the software environment of MATLAB/SIMULINK for further implementation in the simulation framework FLAMES. The model had to be dynamic and require a limited amount of computer capacity. Simplifications have been done so the missile in the developed model only controls in one plane, a plane that rotates in space. This simplification made it possible to denote the model with vector notation in an earth fixed reference frame, the same that is already defined in FLAMES. The model was made dynamic by introducing a filter which lags the system and simulates the dynamic behavior of the missile.