Prof. Ueno researches on guidance and control fields in aeronautical and astronautical engineering. His major is application of optimal control theory to create novel guidance and control laws. The examples of his research themes are minimum time maneuver of formation flight, minimum fuel landing of lunar explorer, minimum energy reorientation of space satellite, and so on. Optimum solutions for nonlinear problems are generally provided using iterative calculation with large amount of computational load. He also researches on new algorithms to generate optimum solutions with light computational load.
Keyword：Artificial satellite, Optimal control