基本信息:
- 专利标题: LASER-GUIDED MINIATURE MISSILE SYSTEM FOR HYBRID THREATS
- 申请号:PCT/TR2021/050545 申请日:2021-06-07
- 公开(公告)号:WO2021251932A1 公开(公告)日:2021-12-16
- 发明人: ATEŞOĞLU, Mustafa Özgür , YÜKSEL, Muhammed , TEKEREK, Ali Şimşek , SEÇKİN UZEL, Öznur Cansu , MUHİDDİNOĞLU, Abdullah Alp
- 申请人: ROKETSAN ROKET SANAYİİ TİCARET A. Ş.
- 申请人地址: Kemalpaşa Mahallesi Şehit Yüzbaşi Adem Kutlu Sokak No:21
- 专利权人: ROKETSAN ROKET SANAYİİ TİCARET A. Ş.
- 当前专利权人: ROKETSAN ROKET SANAYİİ TİCARET A. Ş.
- 当前专利权人地址: Kemalpaşa Mahallesi Şehit Yüzbaşi Adem Kutlu Sokak No:21
- 优先权: TR2020/08783 2020-06-08
- 主分类号: F41G7/22
- IPC分类号: F41G7/22 ; F42B15/01
摘要:
The present invention relates to a laser-guided miniature missile system comprising a launch station (70); and a miniature missile (30) that is provided in said launch station (70), that has an elongated body (32) configured such that it may be launched from a canister (10) or a launch pod (20). The inventive miniature missile system comprises; a remote control station (80) that is connected such that it communicates by means of an RF receiver/transmitter (74) of the launch station (70) accommodated on a mobile vehicle (1) and an opposite RF receiver/transmitter (82); a central controller (72) that triggers a canister (10) or a launch pod (20) such that they launch the miniature missile (30) by means of a pod control member (76) driven by determining a launch command transmitted from the control station (80) to the launch station (70); and a flight controller (38) to the which the central controller (72) is connected such that said central controller (72) ensures signal transmission in a storage mode and that is mounted on the body (32) that activates a flight motor (38) at a predetermined flight motor activation time (t2) by being configured such that it can interrupt the signal communication with the central controller (72) subsequent to a launching moment (t0).
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F41 | 武器 |
----F41G | 武器瞄准器;制导 |
------F41G7/00 | 用于自身推进导弹的方向控制系统 |
--------F41G7/20 | .基于靶位的连续观察 |
----------F41G7/22 | ..跟踪制导系统 |