The future SELENE (SELenological and ENgineering Explorer) mission is planned to make a soft-landing on the lunar surface. The lunar lander is called "SELENE-B." For preliminary terrestrial landing experiments, the flying test bed (FTB) was developed and the first flight experiment finished, which was aimed at validation of the whole FTB flight system. Other experiments are planned for validation of the SELENE-B onboard hardwares, such as sensor systems, and softwares for control systems. In order to validate those systems, it is desirable for the FTB to have the same dynamic characteristics as the SELENE-B. In this paper we are concerned with the controller of the FTB which achieves the SELENE-B model-following system using the FTB. Some numerical simulations are provided to show the effectiveness of the proposed SELENE-B model-following system.
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