Vibration response sensitivity analysis for satellite structures;

The satellite structure is very crucial to the constrains of the weight and deformation due to its special operation environment.

This paper expounds that the carbon fiber composite material has become themain structural material for satellites, Reviews the applications of composite for satellites athome and abroad, further illustrates that the adoption of composite for satellite structures iseven more effective, raises the preliminary viewpoint for the development of compositetechnique for satellites.

and observed thr ough electron microscope in order to verify that satellite droplet structure res ults from the acidity of particle and find out the relationship between them．Re sults indicate that satellite droplets surrounding the particle occur at pH 3.

To test the complex control algorithm for attitude stabilization of multi-body structure satellite with inter-satellite link antennae and antenna tracking and pointing in real-time condition,hardware-in-the-loop simulation(HILS) system of certain large flexible multi-body structure satellite is set up based on xPC target.