| 摘要 |
<p>PROBLEM TO BE SOLVED: To achieve a compact guided control device of a missile with improved position accuracy and response by directly detecting the speed of a gimbal, performing speed control using it, and applying damping when the gimbal is started and stopped. SOLUTION: A missile guided control device calculates a guidance signal required for enabling a missile to perform the proportional navigation. Therefore, a speed s17 of a gimbal 15 is detected by a tachogenerator 19 and a position s16 is detected by a potentiometer 17, the speed s17 and the position s16 are fed back to each adder/subtractor 5 as a gimbal speed signal s5 through a gimbal speed feedback 20 and as a gimbal position signal s2 through a gimbal position feedback 18, respectively, for speed and position control. Therefore, by directly detecting the speed of the gimbal and performing speed control for performing speed damping on activation and stop, position accuracy and response can be improved without applying a large drive torque without being affected by the oscillation of the missile.</p> |
