| 摘要 |
PURPOSE:To miniaturize an optical measuring instrument for a high-speed missile by driving a drive table, fitted with a television camera and high-speed camera, in horizontal and vertical biaxial directions while attaining spatial stabilization. CONSTITUTION:Once an operator selects the position mode on console panel 9, mode change-over switch 11 has its contact placed at side P with mode change-over signal A and driving body 1 moves in proportion to position command B to track a high-speed missile. Next, the rate mode is set via console panel 9. Then, mode change-over signal A places the contact of mode change-over switch 11 at side R to apply the output of integrator 10 to servo unit 12. The attitude change of the high- speed missile is detected by rate gyro 4 and the difference between angle rate signal D and rate command C is applied to integrator 10. As a result, servo unit 12 controls the position of drive table 1. |
