Forrestal application of cavity expansion theory to the model of penetration depth of the aerial bomb trilling into soil, and then, based on the penetrating depth, calculates the size of the crater created by the bomb explosion.

The aerodynamic characteristics of the aerial bombs with strakes and the aerial bombs with swept-back tail wings bave been investigated through experiments in high speed wind tunnel and numerical simulation.

In this paper,we gives out a way of ballistic trajectory fitting of aviation bomb based on ranking Adaptive Genetic Algorithms.

This paper researches on the greatest release air-space of one kind of guided aerial bomb under certain initial release conditions.

This paper simulated the whole guided control system and researched the characteristics such as the trajectories,attack zones and sensitivity to random obstacles of guided aerial bomb by the controlled flight numerical simulation based on the whole system model of the guided aerial bomb.

In order to meet the need of guidance aerial bomb with low-cost,high-precision and high-reliability navigation system,a low-cost integrated navigation system is designed by using flexible IMU and GPS-OEM panel with higher positioning precision and data updating rate.