System for guiding missiles for vehicles and moving targets
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F41G-007/26
G01S-003/786
H04N-005/232
출원번호
US-0317991
(2015-05-13)
등록번호
US-10215533
(2019-02-26)
우선권정보
BE-2014/0450 (2014-06-13)
국제출원번호
PCT/EP2015/060711
(2015-05-13)
국제공개번호
WO2015/189003
(2015-12-17)
발명자
/ 주소
Rondeux, Christian
Balthasart, Pierre
출원인 / 주소
CMI DEFENCE S.A.
대리인 / 주소
Leydig, Voit & Mayer, Ltd.
인용정보
피인용 횟수 :
0인용 특허 :
7
초록▼
An armored vehicle has a turret having a gun; a targeting system which is arranged inside the turret and is provided with a day channel, a night or thermal channel and a laser range-finder, a power control system for controlling the movement of the turret in azimuth and the movement of the gun in el
An armored vehicle has a turret having a gun; a targeting system which is arranged inside the turret and is provided with a day channel, a night or thermal channel and a laser range-finder, a power control system for controlling the movement of the turret in azimuth and the movement of the gun in elevation; a device for guiding missiles using lasers, which generates a laser guiding line; and a turret controller which determines the mode for guiding the missile, wherein the turret has gyrostabilizer for gyrostabilizing the laser-guiding line.
대표청구항▼
1. An armored vehicle comprising: a turret including a cannon;a sight system installed in the turret, the sight system including a day channel, a night or thermal channel, and a laser telemeter, the sight system further including a sight line gyrostabilizer configured to provide a line of sight whic
1. An armored vehicle comprising: a turret including a cannon;a sight system installed in the turret, the sight system including a day channel, a night or thermal channel, and a laser telemeter, the sight system further including a sight line gyrostabilizer configured to provide a line of sight which is gyrostabilized relative to an inertial frame of reference;a power control system configured to command movement of the turret in azimuth and movement of the cannon in elevation;a laser missile guidance device configured to generate a laser guidance line, the laser missile guidance device including a laser line gyrostabilizer configured to gyrostabilize the laser guidance line with respect to the gyrostabilized line of sight provided by the sight line gyrostabilizer such that the laser guidance line is continuously parallel to the gyrostabilized line of sight, the laser line gyrostabilizer comprising a servo-controlled motorized platform rotatable about at least two axes, in elevation and in azimuth; anda turret network controller configured to determine a missile guidance mode,wherein the laser missile guidance device is mechanically independent from the sight system. 2. The armored vehicle of claim 1, wherein the motorized platform comprises a system of mirrors, or a gimbal system. 3. The armored vehicle of claim 1, further comprising: a selector configured to switch the missile guidance mode between a line of sight (“LOS”) mode and an above line of sight (“ALOS”) mode. 4. The armored vehicle of claim 3, wherein the selector is further configured to communicate one or more offset parameters for the elevation and the azimuth using the turret network controller to a motorization device of the turret, the cannon, and the laser missile guidance device, wherein values of the offset parameters are different in LOS mode and ALOS mode. 5. The armored vehicle of claim 1, wherein the laser missile guidance device is servo-controlled with respect a position signal of the gyrostabilized line of sight relative to the inertial reference frame, via at least two feedback loops, in elevation and azimuth, respectively. 6. A missile firing method using the armored vehicle of claim 2, the method comprising: determining sight parameters to engage a target with the day channel or the night channel of the sight system or with a camera of the laser missile guidance device;assigning a desired missile guidance mode of the missile;providing an elevation value for the cannon and an azimuth value for the turret to the power control system;positioning, using the power control system, the turret and the cannon in a firing position;indicating, using the turret network controller, the desired missile guidance mode to the laser missile guidance device;orienting, using the servo-controlled motorized platform with respect to the sight parameters, the laser guidance line so that the laser guidance line is then parallel to the gyrostabilized line of sight; andfiring the missile, which is guided using the laser guidance line. 7. The use of the laser missile guidance device associated with the armored vehicle of claim 1, in a situation involving firing at a moving target, controlled driving of the armored vehicle, vibrations, or strong wind.
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이 특허에 인용된 특허 (7)
Amon Max (Maitland FL) Saccketti Nicholas B. (Tucson AZ), Boresight module.
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