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1. 发明专利

JP2012237563A Target detection apparatus 审中-公开
标题翻译：目标检测装置
公开(公告)号：JP2012237563A
公开(公告)日：2012-12-06
申请号：JP2011104887
申请日：2011-05-10
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： SUETANI TAKANORI , NAKAMURA YUICHI
IPC分类号： G01S3/785 , F41H11/02
摘要： PROBLEM TO BE SOLVED: To provide a target detection apparatus for separating exhaust gas of a flying object from a background and highly accurately detecting the flying object.SOLUTION: The target detection apparatus includes: an S sensor 10 for detecting an angle position θ1 of a first target candidate corresponding to high-temperature gas exhausted from the flying object; an LW sensor 20 for detecting an angle position θ2 of a second target candidate corresponding to the background of which temperature is lower than that of the high-temperature gas; and a target selection processing part 30 for selecting an angle position obtained by removing the angle position θ2 of the second target candidate from the angle position θ1 of the first target candidates out of the angle positions θ1, θ2 of the first and second target candidates acquired by simultaneously detecting a common area by the S sensor 10 and the LW sensor 20, as a target angle position θo.
摘要翻译：要解决的问题：提供一种用于将飞行物体的废气与背景分离并高精度地检测飞行物体的目标检测装置。解决方案：目标检测装置包括：S传感器10，用于检测对应于从飞行物体排出的高温气体的第一目标候选物的角度位置θ1; LW传感器20，用于检测对应于温度低于高温气体的背景的第二目标候选物的角度位置θ2; 以及目标选择处理部30，用于通过从所获取的第一和第二目标候选的角度位置θ1，θ2中的第一目标候选的角度位置θ1中去除第二目标候选的角度位置θ2而获得的角度位置通过S传感器10和LW传感器20同时检测公共区域作为目标角度位置θo。版权所有（C）2013，JPO＆INPIT

2. 发明专利

JP2008137439A Monitor satellite 有权
标题翻译：监控卫星
公开(公告)号：JP2008137439A
公开(公告)日：2008-06-19
申请号：JP2006324104
申请日：2006-11-30
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： MUKAI HISAYUKI , YAMAGUCHI TETSUO , SUETANI TAKANORI , MATSUHIDE TOSHIHISA
IPC分类号： B64G1/66
摘要： PROBLEM TO BE SOLVED: To obtain a monitor satellite capable of exhaustively monitoring an area in a specific latitude in the whole spherical surface of the earth with a small number of satellite instruments orbiting in a low orbit, and performing data transmission to the earth easily.
SOLUTION: This monitor satellite is provided with an infrared sensor 2, a calculating machine 3 processing the detection signal of the infrared sensor 2, a transmitter-receiver 4 giving and receiving data between other artificial satellites flying ahead and behind and itself, and a transmitter 5 performing data transmission to the earth or a flying vehicle. It is configured to fly over the equator approximately at an orbital inclination angle of 0°, and moreover, fly in a position capable of viewing other artificial satellites flying ahead and behind.
COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：为了获得能够利用在低轨道上轨道运行的少量卫星仪器来彻底地监测地球整个球面的特定范围内的区域的监视器卫星，并且执行数据传输到地球很容易
解决方案：该监视器卫星设有红外传感器2，处理红外传感器2的检测信号的计算机3，在其前后飞行的其他人造卫星之间提供和接收数据的发射机 - 接收机4，以及向地球或飞行车辆执行数据传输的发射机5。它被配置为大致以0°的轨道倾斜角度在赤道上飞行，此外，飞行在能够观察其他人造卫星飞行前方和后方的位置。版权所有（C）2008，JPO＆INPIT

3. 发明专利

JP2003279336A Angle-measurement-accuracy measuring apparatus 有权
标题翻译：角度测量精度测量装置
公开(公告)号：JP2003279336A
公开(公告)日：2003-10-02
申请号：JP2002080970
申请日：2002-03-22
申请人： Mitsubishi Electric Corp , Tech Res & Dev Inst Of Japan Def Agency , 三菱電機株式会社 , 防衛庁技術研究本部長
发明人： SUETANI TAKANORI , HYODO SHOZO
IPC分类号： G01B11/26
摘要： PROBLEM TO BE SOLVED: To realize a small angle-measuring-error measuring apparatus for easily preventing a measuring error from being generated due to a parallax between a visible-ray angle measuring device and a specimen.
SOLUTION: A mirror 6 reflects a light beam emitted by a beam combiner 5 to an arbitrary direction regarding a swivel, a depression and an elevation so as to be guided to a half-mirror group 7, the group 7 transmits and reflects the light beam so as to be guided to a position of the specimen and so as to be guided to other specimens, and the mirror 8 guides the light beam to the position of the specimen. Consequently, the small angle-measuring-error measuring apparatus for easily preventing the measuring error from being generated due to the parallax between the visible-ray angle measuring device and the specimen is realized by aligning a detection position coarsely to an extent that a bundle of rays is detected.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：实现一种小角度测量误差测量装置，用于容易地防止由于可见光角度测量装置和样本之间的视差而产生测量误差。解决方案：反射镜6将由光束组合器5发射的光束相对于旋转，凹陷和高度的任意方向反射，以被引导到半反射镜组7，组7透射并反射光束被引导到样本的位置并被引导到其他样本，并且反射镜8将光束引导到样本的位置。因此，通过将检测位置粗略地对准检测位置，可以实现由于可见光角度测量装置和试样之间的视差而容易地防止测量误差的小角度测量误差测量装置，检测到光线。版权所有（C）2004，JPO

4. 发明专利

JPH041583A INFRARED RAY TRACKER 失效
公开(公告)号：JPH041583A
公开(公告)日：1992-01-07
申请号：JP10124890
申请日：1990-04-17
申请人： MITSUBISHI ELECTRIC CORP
发明人： SUETANI TAKANORI
IPC分类号： G01S3/786
摘要： PURPOSE:To stably trace and decide infrared targets in both a highly sensitive area and a low luminance area by providing a function to very the amplification factor of a detecting element amplifier, and making infrared signal receiving sensitivity into high sensitivity extending over a wide area. CONSTITUTION:An infrared signal scanned by an optical system 2 is received with a detecting element 3, and is carried via a signal line 8. A reception signal is switched by an external change-over switch, and is amplified by the detecting element amplifier 4 with the amplification factor controlled by a switch circuit 7, and is processed by a signal processor 5. The switch circuit 10 of the signal processor 5 selects a trace decision circuit 11 in an ordinary operation, and a comparator 12 and an arithmetic circuit 13 in the trace decision circuit 11 perform trace decision processing corresponding to an input signal level. When a result enabling trace to be performed is obtained at the trace decision circuit 11, trace processing is performed by switching the operation to a trace processing circuit 14.

5. 发明专利

JPH0798218A MENACE IDENTIFICATION DEVICE 失效
公开(公告)号：JPH0798218A
公开(公告)日：1995-04-11
申请号：JP24169293
申请日：1993-09-28
申请人： MITSUBISHI ELECTRIC CORP
发明人： SUETANI TAKANORI , KUROKAWA TAKASHI
IPC分类号： F41G3/00 , F41G7/22 , G01B11/02 , G01B11/24 , G01S3/782 , G06T1/00
摘要： PURPOSE:To provide a menace identification device which identifies menace level of air targets and selects the air target of high menace level. CONSTITUTION:An infrared image detector 1 detects an air target and images an infrared image. A servo mechanism 2 scans and points the direction of axis of sight mechanically and electrically. A length measurement processor 3 measures the entire width, height and length of an aircraft of infrared image. An aspect menace identification processor 4, with the use of the length value measured by the length measurement processor 3, identifies the menace level of the air target based on the entire width, height or length.

6. 发明专利

JPH11304593A INFRARED RADIATION DETECTING APPARATUS 失效
公开(公告)号：JPH11304593A
公开(公告)日：1999-11-05
申请号：JP10781198
申请日：1998-04-17
申请人： MITSUBISHI ELECTRIC CORP
发明人： SUETANI TAKANORI , FURUYA AKIRA
IPC分类号： G01J5/02
摘要： PROBLEM TO BE SOLVED: To realize an infrared radiation detecting apparatus without using an expensive infrared detector of low noise, in an infrared detecting apparatus mounted on a flying body. SOLUTION: An infrared radiation window 1 transmits infrared radiation. An infrared optical system 2 condenses infrared radiation and forms an image on an infrared detector 3, which detects infrared radiation and performs photoelectric conversion. A cabinet 4 releases airtight between the infrared optical system 2 and the outside, shields the infrared detector 3 from the outside, and retains the infrared window 1, the infrared optical system 2 and the infrared detector 3. An air filter 5 prevents permeation of foreign matter when cooling air is taken in from the outside. A moisture absorber 6 absorbs water vapor involved when the cooling air is taken in from the outside. By this constitution, the optical system is cooled while thermally insulated from other parts.

7. 发明专利

JPH09230021A TARGET DETECTING DEVICE 失效
公开(公告)号：JPH09230021A
公开(公告)日：1997-09-05
申请号：JP3664496
申请日：1996-02-23
申请人： MITSUBISHI ELECTRIC CORP
发明人： SUETANI TAKANORI
IPC分类号： F41G3/00 , F41G7/20 , G01S3/782
摘要： PROBLEM TO BE SOLVED: To select and detect a flying body only as a target without detecting the gound or cloud. SOLUTION: An optical system 1 collects infrared rays of wavelength band containing the vicinity of 2.7μm and images them on an infrared detector 3. A narrow band filter 2 transmits an infrared band of center wavelength in the vicinity of 2.7μm. The infrared detector 3 generates detected signals by photo-electric transferring of infrared rays of wavelength band containing the vicinity of 2.7μm. A target extractor 6 selects a target from the detected signals. A tracking error computer 7 knows an angle between a visual line and a target position, and computes a tracking error quantity corresponding to it. A visual line controller 9 controls to drive a visual line control mechanism 8 so as to scan and orient the visual line. A target angle gauge 10 addingly processes the angular position of the visual line obtained by the visual line control mechanism 8 and the angle between the visual line obtained by the tracking error computer 7 and the target position, so as to obtain the relative angle of the target in an inertia space.

8. 发明专利

JP2000171305A INFRARED RAY DETECTING DEVICE 失效
公开(公告)号：JP2000171305A
公开(公告)日：2000-06-23
申请号：JP34409498
申请日：1998-12-03
申请人： MITSUBISHI ELECTRIC CORP
发明人： SUETANI TAKANORI
IPC分类号： G01J1/02 , G01J5/02
摘要： PROBLEM TO BE SOLVED: To provide a low-noise infrared ray detecting device, without the use of an expansive low-noise infrared ray detector, in the infrared ray detecting device loaded on aircraft. SOLUTION: An infrared window 1 transmits infrared ray. An infrared optical system 2 focuses an image on an infrared ray detector 3 by converging the infrared ray. The infrared detector 3 detects and transducer photoelectrically the infrared ray. A casing 4 has a structure comprising a release area such as a hole formed in a portion other than the surface of the infrared window 1 of a bulkhead for sealing the infrared optical system 2 by shielding it from surroundings, and the bulkhead also disposed in a position for sealing the infrared detector 3 by shielding it from the ambient atmosphere in the infrared optical system 2 and from the surroundings, so that the infrared optical system 2 releases airtightness while the infrared detector 3 is kept airtight, and so that the casing 4 supports the infrared window 1, the infrared optical system 2 and the infrared detector 3. A thermal insulator 5 is mounted on the bulkhead of the casing 4 so as to isolate adiabatically the interior, wherein the infrared window 1 and the infrared optical system 2 are housed, from the surroundings. An exhauster 6 is disposed in the airtightness release area of the casing 4 so as to exhaust the air from the interior, wherein the infrared window 1 and the infrared optical system 2 are stored, thereby cooling the infrared optical system 2.

9. 发明专利

JPH06109400A GUIDANCE APPARATUS 失效
公开(公告)号：JPH06109400A
公开(公告)日：1994-04-19
申请号：JP25960392
申请日：1992-09-29
申请人： MITSUBISHI ELECTRIC CORP
发明人： SUETANI TAKANORI
IPC分类号： F41G7/22 , F42B15/01 , G01S3/782 , G01S3/786 , H04N5/30 , H04N7/18
摘要： PURPOSE:To realize a guided apparatus for selecting and guiding one of a combat warship and a noncombat warship as a target. CONSTITUTION:An incident light passed through an optical window 1 is collected by an optical system 2, suspended by a sensor suspension unit 4, and introduced into an image sensor 3 driven by a sensor driver 5 to be sensed. A chimney position warship type identifier 9 identifies and decides a noncombat warship when a ratio of a length of a hull center line of a chimney position on a screen to be imaged to an entire length is 4 or less and a combat warship when it is 10 or more to so process that either one type warship is a target. A signal processor 6 searches and tracks the target sorted by the identifier 9. A signal cable 7 transmits a signal between the units. A housing 8 protects the above device against the outer field.

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