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.

According to the SINS/GPS guided bomb of the tilt-sport model,a kind of the guided bomb of the tilt- stablize loop design method based on classic controling theories is introduce in this paper.

By combining project ballistics with on-line neural network,a new control method is gained for simple guided-bomb s control system.

Under large angle of attaek and high altitude,serious coupling problem exists between simple guided-bomb s yawing channel and rolling channel.

Based on the guidance for a simply guided bomb, chief factors having impact on the range and accuracy of the bomb were analyzed.

As a low cost guidance technology, the simplified guidance technology is a new approach to improve rocket s performance.

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.