Desenvolvimento de uma simulação Monte Carlo para míssil ar-ar guiado a laser

Abstract

The objective of this work is to develop a Monte Carlo Simulation for a laser guided air-to-air missile in order to determine the requirements of the main missile subsystems without making its construction unfeasible while at the same time ensuring a reasonable kill probability, taking into account errors and disturbances from sensor readings and errors in actuator execution and missile propulsion. It was used as basis for the development of the simulation the undergraduate work [1] in this way some of the suggestions suggested by the mentioned work were implemented. The simulation considered the insertion of Run-to-Run and in-Run errors in the following subsystems: aerodynamics, propulsion, navigation, self-steering, actuator; and detecting the initial position and speed of the target. In addition, we have studied cases where there are limitations of data reading such as position and target tracking speed by the auditor and the saturation distance of the auditor, such limitations model what happens in a real flight.