| 摘要 |
PROBLEM TO BE SOLVED: To provide an altitude-control simulator of a combination of an actual rocket engine and an airframe model mounted therewith. SOLUTION: An altitude-control simulator comprises an altitude controller 21 which receives an altitude command and outputs a combustion-pressure request value, a rocket engine 22, 23 and 24 which combusts according to the combustion-pressure request value to output combustion pressure, and an airframe model 25 which receives the combustion pressure and outputs the altitude data of an airframe mounted with the rocket engine. The altitude controller 21 effects feedback control of receiving the altitude data to set it meeting the altitude command, while the rocket engine effects feedback control of receiving the combustion pressure to set it meeting the combustion-pressure request value. |
