The trajectory planning for spacecraft formation reconfiguration was modeled as a Multi-objective Optimization Problem and a niched evolutionary algorithm was proposed to find the Time-Fuel Pareto optimal frontier.

Application of stochastic trajectory model in tail-nozzle SRM flow field numerical simulation;

It is suggested that the part ide- motion- resolution trajectory model is efficient for simulating the dynamic behavior of circulating fluidized beds.

In order to provide analysis results for fault diagnosis in a tailpipe nozzle to make some suggestions,twophase flow field is studied for a tailpipe nozzle by using the trajectory model and finite volume method to obtain the gas temperature and Mach number distributions,and to simulate the collision between the wall and different size particles under different total pressures.