2001 年 49 巻 569 号 p. 197-200
The essential benefit of HardWare-In-the-Loop (HWIL) simulation can be summarized as that the performance of autopilot system is evaluated realistically without the modeling error by using actual hardware such as seeker systems, autopilot systems and servo equipments. The most important requirement at the HWIL simulation test is to set the homing seeker at the 3-axis gimbals center of the flight motion table. But, because of the various reasons such as the length of the homing seeker, the structure of the flight motion table and the shape of attachments, this requirement on setting is not able to be satisfied. In this paper, the effect of this position error on the guidance and control system performance is analyzed and evaluated.