Six-Degree-Freedom Full-Quantity Mathematical Modeling and Simulation of Launch Vehicle Control System

摘要

This paper selects a type of launch vehicle as research background and its control system as research object. The six-degree-freedom full-quantity mathematical modeling and simulation method of the flying launch vehicle have been fully discussed in the paper. The technology brought forward in this paper utilizes comparative integrated and accurate mathematical models and analyzes simulation results of different interferences, thus greatly increases the reliability and precision of simulation. It can be taken as a valuable reference to other integrative simulations of complex systems.