A multiple ballistic model of constant physical parameter is established and a multiple ballistic revised model of continuous and non continuous physical parameter is educed.

On the basis of further studying and analyzing the trajectory trait,the paper has constructed fold line trajectory model which is correspond to the flying character of red land laser terminal-guided projectile when firing at near distance.

Impulse correction scheme of a terminal correction rocket was put forward,and the trajectory model was established.

It constructed the anti-ship whole trajectory model with interferences,then designed the flight test region by setting missile parameters,contrasted the simulation test with the actual range test,and verified the rationality and superiority of the scheme.

On the basis of determining the ballistic model and selection method of time on target program,the structure design and user interface design of software are described.

Focused on the tracking precision problem caused by mismatch of tracking model with the real movement of modern anti-ship missile in current algorithms,a maneuvering target tracking algorithm based on ballistic model was presented by analyzing the ballistic characteristics of anti-ship missile and the relationship between missile dynamics and the kinematics.

The contact boundary between the large-diameter thin-walled cylindrical shell structure with foundation bed can be treated as a new numerical model-spring-element model, and large-scale common finite element software-ANSYS can be used to compute and anylyse the deformation, internal force and the base stress of thin-walled cylindrical structure through second development.