Considering the characteristics of a guided bomb, the paper establishes a series of sideling coordinate systems.

Aim To study the effect of aerodynamically stabilized seeker dynamics on guided bomb system analysis.

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.

The nonlinear dynamic model of a guided bomb can be dealt with a nonlinear time variable system based on the differential geometry and advanced control theory, which is separated four layers: centroid, velocity, attitude, angular rate.

For problems of sample data processing in IMU of guided bombs, a novel method using adptive wavelet based on lifting scheme was proposed in this paper.