Visual dynamics simulation for adapters separation of missile launching

The process of the adapter separating from missile plays an important role in safety and reliability launching, which involves complex dynamics calculations. In order to guarantee successfully launching missile, this article was concerned with whole system presented a novel calculation method visual simulation software analyze separation. models including coordinate system, kinematic equations, forces acting on are established. random factors their distribution law that greatly influence separation analyzed, confidence intervals estimated by using Monte Carlo method, algorithm for calculating distance between adapter, wing, tail rudder is proposed. Visual analyzing designed, gathers modeling, solving, analytical processing. Finally, numerical result given verify validity correctness proposed affecting adapters launching. paper can provide support design