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公开(公告)号：WO2023033939A1
公开(公告)日：2023-03-09
申请号：PCT/US2022/037048
申请日：2022-07-14
Applicant: RAYTHEON COMPANY
Inventor： FLEDER, Charles Edward , GENTILMAN, Richard L. , WOOLF, Martin A.
Abstract: A guidance system for a missile performs a method for guiding the missile. The guidance system includes a target detector (202) and a window (208) between a target (202) and the target detector. The window including a first pane, a second pane and a channel between the first pane from the second pane. Radiation (210) from the target passes through the window including the first pane, the second pane and the channel to be detected at the target detector. A gas is transported through the channel between the first pane and the second pane to control a temperature of the window.
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公开(公告)号：WO2022225598A1
公开(公告)日：2022-10-27
申请号：PCT/US2022/016647
申请日：2022-02-16
Applicant: RAYTHEON COMPANY
Inventor： BRAUNREITER, Dennis , FREEMAN, Matthew , DOUGLAS, Dave S. , BONTRAGER, Paul , MORALES, Anibal
Abstract: A system and method for tracking a target. An acquisition and track sensor (ATS) includes a wide field of view (FOV) camera system continuously capturing an image of the target. The ATS can be a mid-wave infrared tracker. The ATS identifies the target for tracking and cues the target for tracking. A fine track sensor (FTS) includes a narrow FOV camera system. The FTS can be a short-wave infrared tracker. The FTS continuously re-centers the narrow FOV around the target after the target is cued by the ATS. The ATS and FTS include independent steering mechanisms for respective camera systems.
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公开(公告)号：WO2021257031A1
公开(公告)日：2021-12-23
申请号：PCT/TR2021/050574
申请日：2021-06-14
Applicant: ROKETSAN ROKET SANAYİİ TİCARET A. Ş.
Inventor： ATEŞOĞLU, Mustafa Özgür , MUHİDDİNOĞLU, Abdullah Alp , GÖRÜR, Bilge Kaan , ALTINTAŞ, Oğuz Han
Abstract: The present invention relates to a distributed missile system having multiple miniature missile units (n) comprising the following; an elongated body (10) with a warhead (11); a drive motor (12) fixed to the body (10); a fin (14) that is provided in the body (10) and that rotates the body (10) towards a predetermined course during the cruise by being driven with the drive motor (12) and a controller (40) connected to the drive motor (12) to control the fin (14) position. The missile system comprises at least one relative awareness sensor (30) that scans the outer periphery of the body (10) by collecting 360° environmental awareness data (v) and transmits a signal to the controller (40).
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公开(公告)号：WO2021251932A1
公开(公告)日：2021-12-16
申请号：PCT/TR2021/050545
申请日：2021-06-07
Applicant: ROKETSAN ROKET SANAYİİ TİCARET A. Ş.
Inventor： ATEŞOĞLU, Mustafa Özgür , YÜKSEL, Muhammed , TEKEREK, Ali Şimşek , SEÇKİN UZEL, Öznur Cansu , MUHİDDİNOĞLU, Abdullah Alp
Abstract: 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).
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公开(公告)号：WO2021091601A2
公开(公告)日：2021-05-14
申请号：PCT/US2020/041920
申请日：2020-07-14
Inventor： FREY, Jr., Robert D. , AFFLECK, Maxwell L. , BATCHELDER, Jason H. , CULLEN, Joseph P. , ROBICHAUD, Matthew H.
IPC: F41G7/26 , F41G7/24 , F41G7/22 , F41G7/2246 , F41G7/226 , F41G7/2293 , F42B10/60 , F42B15/01 , F42B15/105 , G01J1/0214 , G01J1/0219 , G01J1/0252 , G01J1/0407 , G01J1/0422 , G01J11/00
Abstract: An optical seeker assembly having an optical detector located within the wing or canards of a precision guided munition. The optical seeker provides on-wing processing that generates low bandwidth detection data that can be easily transferred to a primary CPU located within the main body or fuselage of the precision guided munition. The on-wing processing reduces or eliminates the need for optical fibers extending between an optical wedge and an optical detector to reduce the likelihood of optical fibers from impeding in the mechanical deployment of the wing and reduces losses. The reduction or elimination of optical fibers between the optical wedge and the optical detector further enables the optical detection assembly to have a higher pixel ratio or transmitting raw data between the wedge and the detector by sending sampled detection data across a low bandwidth link to a CPU in the main body.
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Patent Agency Ranking
公开(公告)号：WO2020193881A1
公开(公告)日：2020-10-01
申请号：PCT/FR2020/050214
申请日：2020-02-07
Applicant: MBDA FRANCE
Inventor： FORMOSO, Mathias , JEAUNEAU, Vincent , KOTENKOFF, Alexandre , BANDINI, Alain
IPC: F41G3/18 , B64C39/02 , F41G7/22 , F41H7/00 , F42B12/36 , F42B12/40 , G05D1/12 , F41G7/32 , F41G7/30
Abstract: Le système de neutralisation (1) comporte un drone (2) configuré pour pouvoir s'approcher en volant d'une cible et émettre au moins des informations de position de la cible, le système de neutralisation (1) comportant également au moins un missile (6) apte à être guidé vers la cible afin de la neutraliser et au moins un poste de contrôle (8), le poste de contrôle (8) comprenant une unité de réception (9B) apte à recevoir au moins les informations de position émises par le drone (2) et une unité d'affichage (10A) apte à présenter ces informations à un opérateur, le missile (6) étant configuré pour pouvoir être guidé vers la cible à l'aide desdites informations de position reçues par le poste de contrôle (8).
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7.发明申请
公开(公告)号：WO2020025518A1
公开(公告)日：2020-02-06
申请号：PCT/EP2019/070315
申请日：2019-07-29
Applicant: AIRBUS DEFENCE AND SPACE SAS
Inventor： HENNART, Florent
IPC: G01S19/25 , G01S19/47 , G01S19/26 , G01S19/14 , G01S19/49 , G01S19/24 , F42B10/26 , F42B15/01 , F41G7/22 , F41G7/30 , F41G7/34
Abstract: L'invention concerne un dispositif (400) de localisation d'un objet mobile susceptible de subir une dynamique de rotation sur lui-même. Le dispositif comporte un récepteur (410) d'un système de positionnement par satellites, une centrale inertielle (420), et un module hybride de navigation (430). Le module hybride de navigation (430) est configuré pour modéliser d'une part le mouvement d'une antenne (54) du récepteur (410), et d'autre part le mouvement d'un satellite, afin d'estimer une valeur représentative de l'effet Doppler subi par le signal émis par le satellite et reçu par l'antenne. Cette valeur est communiquée à un module d'acquisition (411) du récepteur afin de faciliter une ré-acquisition du signal du satellite suite à une perte du signal provoquée par le mouvement de rotation de l'objet mobile. Le mouvement de l'antenne (54) est notamment estimé grâce à la connaissance de la distance séparant l'antenne d'un centre d'inertie de l'objet mobile.
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公开(公告)号：WO2019217971A1
公开(公告)日：2019-11-14
申请号：PCT/US2019/032040
申请日：2019-05-13
Applicant: FENIX GROUP, INC.
Inventor： PETERSON, David , SCHANER, Stefan
Abstract: Systems and methods for deploying smart munitions may provide targeting metadata generated by surveillance networks to munitions deployment and guidance systems for smart munitions. Targeting metadata may be received by a conduit system and automatically processed to generate guidance and deployment data actionable by a munitions deployment platform.
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公开(公告)号：WO2018136116A1
公开(公告)日：2018-07-26
申请号：PCT/US2017/049399
申请日：2017-08-30
Applicant: RAYTHEON COMPANY
Inventor： TITUS, Christopher J.
Abstract: Methods and apparatus for variable time sampling of optical pulses by a unit cell are disclosed. The methods may include detecting whether an amplitude of an optical pulse incident on one or more photo-detecting elements exceeds a sampling threshold, and while the pulse amplitude remains above the sampling threshold, iteratively sampling the optical pulse at a sampling rate that varies based on changes in the pulse amplitude.
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公开(公告)号：WO2017127144A1
公开(公告)日：2017-07-27
申请号：PCT/US2016/058802
申请日：2016-10-26
Applicant: RAYTHEON COMPANY
Inventor： RONCONE, Ronald, L. , LICKSON, Raymond, S. , PETERSON, Eric, X.
IPC: F41G7/22
CPC classification number: F41G7/226 , F41G7/2293 , G01S3/782 , G02B5/0278 , G02B5/285 , G02B13/18
Abstract: A dual-band semi-active laser (SAL) sensing system incorporating a dual-passband filter (204). According to one example, a semi-active laser sensing system includes a detector assembly (208) and an aperture lens (202). The SAL sensing system further comprises a dual-passband filter (204) having a stopband, a first passband and a second passband, the first and second passbands being distinct and non-overlapping and spectrally separated from one another by a portion of the stopband, the filter being configured to receive the electromagnetic radiation from the aperture lens and to filter the electromagnetic radiation to pass a first wavelength range within the first passband and a second wavelength range within the second passband. The SAL sensing system further includes a lens assembly (206) configured to receive the first and second wavelength ranges from the filter and to focus the first and second wavelength ranges onto the detector assembly.
Abstract translation: 包含双通带滤波器（204）的双频带半主动激光（SAL）感测系统。 根据一个示例，半主动激光感测系统包括检测器组件（208）和孔径透镜（202）。 SAL感测系统还包括具有阻带，第一通带和第二通带的双通带滤波器（204），第一和第二通带是不同的并且不重叠并且在频谱上彼此隔开一部分阻带， 所述滤波器被配置为接收来自所述孔径透镜的电磁辐射并过滤所述电磁辐射以通过所述第一通带内的第一波长范围和所述第二通带内的第二波长范围。 SAL感测系统还包括透镜组件（206），该透镜组件（206）被配置为接收来自滤波器的第一和第二波长范围并将第一和第二波长范围聚焦到探测器组件上。
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