| 摘要 |
<p>PURPOSE:To directly evaluate performance of a missile system for controlling a body motion by deflecting a direction of thrust of a propulsion unit by a closed loop (hardware-in-the-loop) test. CONSTITUTION:A TVC machine 1 with a movable nozzle 2 is supported to a test bench 4 through component force measuring units 7, and component forces acting a body by thrust deflected by a steering angle command based on a guide command are output by the units 7. A body motion is calculated by a body motion calculating software of a calculator 12 by using it. Guide control performance is evaluated by a guide control calculator 22.</p> |
