Design Of Simulation Software On Missile Flight

Modern military struggle highlights the growing role of missiles, military power between the state and national political and economic competition is particularly prominent. This paper analyzes the process of missile flight dynamics and kinematics, the use of Qt Creator programming tools to implement a missile flight simulation, and analysis system using the model of the missile's flight data analysis, the error is given to correct model.Base on missile kinematics model and the theory of robust control, this thesis simulated the flight of missile and guidance and control system. The main research works of this thesis are described as follows:1. Build and compile database of scientific computing applications of GSL, and using mathematical tools GSL to solve the missile model. Meanwhile, in the Linux environment, complete painting dynamics flight data display.2. Design software architecture of simulation on a missile flight, and based on robust control theory, achieved flight simulation software of the missile flight. Verify the system's basic functionality and usability through the simulation of a BTT missile.3. In the Linux development environment, design a drawing function class and inertial system error handling class, use Qt Creator development tool achieve the model analysis subsystem of inertial component test systems.