Study of Flying Control Computer Based on Plug-and-Play Method

摘要

The applications of plug and play (PnP) method to flying control computer for aerospace launch vehicle is studied, and the plug-and-play model of flying control computer is discussed. Then the PnP design scheme of flying control computer is presented, also the validation experiment is carried through. At last, a simple demonstration system is built, and the research method is tested and analyzed, The test result shows that the above PnP design scheme is correct and will support the future aerospace launch vehicle for upholding the responsive ability.