| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a missile guidance system that can further improve portability and operability of a missile to be launched by, in particular, a portable launcher in a controllable propulsion direction. <P>SOLUTION: In the missile guidance system, a guidance device 30 generates a guidance command to bring a flight direction Df detected by a flight direction detection part such as a camera part 21 close to an eyesight direction De of an operator 40 obtained from an eyesight measurement part 22, and transmits the guidance command to a missile 10. In this way, the operator 40 can substantially make the missile 10 fly onto the line of sight (LOS) only by seeing a target 50. <P>COPYRIGHT: (C)2013,JPO&INPIT |
