| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 241 | Autopilot | US26697852 | 1952-01-17 | US3011738A | 1961-12-05 | SKRAMSTAD HAROLD K; HART JOHN A |
| 242 | Autopilot | US75785258 | 1958-08-28 | US3094299A | 1963-06-18 | BOND ROBERT W; LADD JOHN H; ROBERTS JR ROY L; KELLER GEORGE R; MARKEY HAROLD G |
| 243 | 엔에프씨를 이용한 시간 검증 기반 오티피 생성 방법 | KR1020140146124 | 2014-10-27 | KR101537485B1 | 2015-07-16 | 김종서 |
| 본발명의엔에프씨를이용한시간검증기반오티피생성방법에따르면, NFC(Near Field Communication)모듈을구비한사용자의무선단말에서실행되는방법에있어서, 상기 NFC모듈을통해적어도 1회통신한 OTP카드의메모리에상기무선단말의기기인증을위해지정된고유번호를기록하고, 상기 OTP카드의메모리에상기고유번호를기록한등록시간을확인하여상기무선단말의지정된저장영역에저장하고, 상기 OTP카드를통해거래용OTP 생성시, 지정된서버를통해상기등록시간과고유번호를이용하여동적생성된기기인증용OTP를확인한후 상기 NFC모듈을통해상기확인된기기인증용OTP를상기 OTP카드로전송하여기기인증을요청하고, 상기 OTP카드를통해상기무선단말이인증된경우에타이머를통해실시간확인된시간값을포함하는씨드값을구성하여상기 NFC모듈을통해상기 OTP카드로전송하고, 상기 NFC모듈을통해상기 OTP카드로부터상기시간값에대한검증오류결과를수신하거나또는상기검증된시간값을근거로동적생성된거래용OTP를수신하고, 상기거래용OTP가수신된경우, 상기수신된거래용OTP를출력하며, 상기 OTP카드는, 상기고유번호를기록시 상기고유번호를기록한등록시간을저장하며, 최초의거래용OTP를생성시 상기최초의거래용OTP를생성한생성시간을저장하며, 이후의거래용OTP를생성시 이전에생성된거래용OTP에대한생성시간을확인하고, 상기거래용OTP를생성하기위해수신된시간값과저장된생성시간을비교하여상기수신된시간값이이전에저장된생성시간이후의시간으로인증된경우상기거래용OTP를동적생성하고상기거래용OTP를생성한생성시간을갱신저장한다. | ||||||
| 244 | 터치패널을 이용한 회전익 항공기 자동조종장치 및 자동조종방법 | KR1020130107692 | 2013-09-09 | KR1020150029067A | 2015-03-18 | 강영신; 박범진; 조암; 유창선; 김중욱 |
| 터치패널을 이용한 회전익 항공기 자동조종장치 및 자동조종방법에 대하여 개시된다. 회전익 항공기 자동조종방법은 콘솔부 메인 화면의 임무조종 선택창 생성단계, 임무조종 선택창의 버튼이 활성화 되는 단계와 임무조종 선택창의 버튼을 클릭하는 단계, 해당버튼에 대한 업무를 수행하는 단계로 구성되며, 임무조종 선택창의 버튼을 터치함으로써, 항공기가 해당버튼에 대응하는 임무를 수행하도록 구성된다. 이는, 명령버튼을 터치하기 때문에, 조종사가 실수로 스틱을 건드릴 가능성이 줄어 들어 사고 등이 일어나는 문제를 줄여줄 수 있으며, 업무의 효율성을 향상 시킬 수 있다.
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| 245 | 엔에프씨를 이용한 시간 검증 기반 오티피 생성 방법 | KR1020140146117 | 2014-10-27 | KR1020140147782A | 2014-12-30 | 김종서 |
| 본발명의엔에프씨를이용한시간검증기반오티피생성방법에따르면, NFC(Near Field Communication)모듈을구비한사용자의무선단말에서실행되는방법에있어서, 상기 NFC모듈을통해적어도 1회통신한 OTP카드의메모리에상기무선단말의기기인증을위해지정된고유번호를기록하고, 상기 OTP카드의메모리에상기고유번호를기록한등록시간을확인하여상기무선단말의지정된저장영역에저장하고, 상기 OTP카드를통해거래용OTP 생성시, 상기무선단말의지정된저장영역에저장된등록시간과상기고유번호를이용하여기기인증용OTP를동적생성한후 상기 NFC모듈을통해상기생성된기기인증용OTP를상기 OTP카드로전송하여기기인증을요청하고, 상기 OTP카드를통해상기무선단말이인증된경우에타이머를통해실시간확인된시간값을포함하는씨드값을구성하여상기 NFC모듈을통해상기 OTP카드로전송하고, 상기 NFC모듈을통해상기 OTP카드로부터상기시간값에대한검증오류결과를수신하거나또는상기검증된시간값을근거로동적생성된거래용OTP를수신하고, 상기거래용OTP가수신된경우, 상기수신된거래용OTP를출력하며, 상기 OTP카드는, 상기고유번호를기록시 상기고유번호를기록한등록시간을저장하며, 최초의거래용OTP를생성시 상기최초의거래용OTP를생성한생성시간을저장하며, 이후의거래용OTP를생성시 이전에생성된거래용OTP에대한생성시간을확인하고, 상기거래용OTP를생성하기위해수신된시간값과저장된생성시간을비교하여상기수신된시간값이이전에저장된생성시간이후의시간으로인증된경우상기거래용OTP를동적생성하고상기거래용OTP를생성한생성시간을갱신저장한다. | ||||||
| 246 | 자동감김장치를 이용한 자동인출식 도어 및 이를 구비한 냉장고 | KR1020110139402 | 2011-12-21 | KR1020130071919A | 2013-07-01 | 김명환; 유대현 |
| PURPOSE: An automatically extractable door using an automatic winding device and a refrigerator having the same are provided to prevent a wire from becoming twisted or cut because the wire is wound around a winding device and stored inside the winding device and to improve durability. CONSTITUTION: An automatically extractable door using an automatic winding device comprises a drive unit, a wire (30), and an automatic winding device (100). The drive unit is installed on the inner side of a door (4) of a refrigerator and automatically opens and closes the door. The wire supplies power to the drive unit. When the door is opened, the wire is unwound from the automatic winding device unwinds the wire. When the door is closed, the wire is wound around the automatic winding device. The automatic winding device comprises a case (110), a leaf spring (130), and a winding shaft (120). The case receives the wound wire therein. The leaf spring has elastic restoring force. One end of the leaf spring is fixed to the winding shaft in the the case. | ||||||
| 247 | 증기발생기의 물상자내에서 작동하기 위한 원격 자동 조종장치 | KR1019820004477 | 1982-10-05 | KR100026538B1 | 1988-11-14 | 베르나르드레부크; 게오르게끌라르 |
| 248 | Automatic pilot apparatus | US10870319 | 2004-06-17 | US20050056730A1 | 2005-03-17 | Takashi Nagayama; Hiroshi Yoneda |
| Refurbishment work on installation of an automatic pilot apparatus into an aircraft is significantly simplified. An automatic pilot apparatus 1 which is installable in an aircraft comprises: a navigation device 2 to guide the aircraft along a predetermined flight path; actuators 3a to 3d to drive control surfaces of the aircraft; a flight computer 4 to control the actuators 3a to 3d; a case body 10 to contain the navigation device 2, the actuators 3a to 3d, and the flight computer 4; a fixing member to fix the case body 10 to a pilot seat S of the aircraft; and additional rods 30a to 30d to transmit driving forces of the actuators 3a to 3d to the control surfaces. | ||||||
| 249 | Pupillomètre automatique entièrement statique | EP90401082.4 | 1990-04-20 | EP0395478A1 | 1990-10-31 | Hennequin, Jean-Claude; Massart, Christian |
Le pupillomètre comporte un boîtier (2) avec une face frontale (2a) qui correspond, en position, à une monture de lunettes. Le pupillomètre comporte un axe principal (3), perpendiculaire à la face frontale (2a) et équidistant des yeux du sujet. Un plan d'horizon, perpendiculaire au plan de figure, passe par l'axe principal (3) et les yeux du sujet. Dans le boîtier est disposée une lentille maîtresse (4) et un point source lumineux (7) au foyer de la lentille et sur l'axe optique principal (3). Le point source (7) crée, au centre des yeux du sujet, des reflets cornéens, dont la lentille (4) donne des images virtuelles. Ces images virtuelles forment objets réels pour une optique d'objectif (5) qui forme une paire d'image réelle sur une échelle de lecture (6) formée d'une ou plusieurs barrettes à transfert de charge, photosensibles. L'analyse séquentielle du dispositif (6) repère les éléments de barrettes où se sont formées les images par les rangs de ces éléments. |
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| 250 | MODULAR VIAL AUTOSAMPLER | PCT/US1995008307 | 1995-07-03 | WO1996001994A1 | 1996-01-25 | TEKMAR COMPANY; RAO, Prabhakar, P.; LEWIS, Edmund, T.; GREEN, Thomas, B. |
| A modular vial autosampler (10) has a storage area (14) for vials (42, 44) containing samples to be analyzed and at least one modular sampling station (20, 22). A vial transfer mechanism (28) lifts a sample vial from the storage area (14), moves it to a station (18) for identification and then to a sampling station (20, 22), and under central control activates the sampling station (20, 22) for obtaining a sample for analysis. The vial transfer mechanism (28) is movable in x, y and z directions to capture and move a selected vial (20, 22). The autosampler (10) has a series of valves (P5, X6, X4) operable under central control to selectively introduce two different standards (240, 242) into the sample, and after obtaining the sample, for rinsing and purging the conduits or lines and needles to reduce sample carryover. The modular vial autosampler (10) includes controls to selectively sample either a gas or a liquid using many of the same components. | ||||||
| 251 | Dispositif de pilotage automatique pour aérodynes | EP94401074.3 | 1994-05-11 | EP0628898A1 | 1994-12-14 | Pierson, Benoit; Guiol, Georges; Limon, Florence |
Le dispositif selon l'invention fait intervenir au moins un calculateur numérique (1) recevant des informations émanant d'un ensemble de capteurs, et assurant la commande d'actionneurs agissant sur les gouvernes, ce calculateur (1) comprenant au moins un module de calcul (10) autonome disposant de ressources matérielles et logicielles aptes à assurer le pilotage selon l'un quelconque des trois axes de pilotage, ce module (10) disposant de moyens pour se rendre spécifique d'un axe déterminé parmi lesdits axes de pilotage, et des moyens de connexion (5) pour se connecter aux capteurs (4) et aux actionneurs (2,3) correspondant audit axe déterminé. Il s'applique notamment au pilotage automatique d'un hélicoptère. |
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| 252 | CORRECTION OF ERRORS IN AUTOPILOTS | EP88903897.0 | 1988-05-05 | EP0357660A1 | 1990-03-14 | BOOTH, Thomas, Brindley |
| Système (1) répondant à des entrées (2) en parallèle avec un estimateur d'état (4). Le système de commande (6) fournit les entrées (2) en réponse à des entrées d'état ordonnées (14) et à des entrées de l'estimateur d'état. Un vecteur (f) de perturbations externes intervient sur le système (1) de sorte que les valeurs observées des variables d'état sont différentes des valeurs estimées. Les valeurs estimées et mesurées sont comparées (8) pour donner un signal d'erreur (9). Les valeurs d'erreur sont introduites dans un correcteur d'état ordonné (11) qui calcule l'erreur qu'aurait la variable d'état ordonné dans l'état stable, et l'applique dans le sens opposé pour augmenter l'état ordonné d'entrée (14). S'il faut corriger plus d'une variable d'état, la correction est directement appliquée aux entrées de commande par utilisation du correcteur multi-état, dans lequel les erreurs d'état stable sont utilisées pour trouver les entrées de commandes qui provoqueraient les erreurs, et ensuite une correction est appliquée aux entrées de commande. | ||||||
| 253 | PATH PLANNING AUTOPILOT | EP13787579 | 2013-05-08 | EP2847643A4 | 2016-06-22 | PEAKE JOHN W; PLEINES STEPHAN |
| A path planning autopilot guides vehicles efficiently even when they are far from a desired path. | ||||||
| 254 | Automatic pilot pitch angle compensation | EP10155029.1 | 2010-03-01 | EP2224306A3 | 2014-08-13 | Blechen, Frederick Charles Henry |
A method, apparatus, and computer program product are present for operating an aircraft. Responsive to a command (700) to hold an altitude of the aircraft, an adjustment to a pitch angle of the aircraft needed to substantially maintain the altitude of the aircraft is identified (702) using a lift for the aircraft to form an identified adjustment to the pitch angle to reduce altitude deviations from at least one of a change in configuration of a number of flight surfaces and changes in wind. The pitch angle of the aircraft is adjusted (704) using the identified adjustment during flight.
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| 255 | Autopilot for flying object | JP17872182 | 1982-10-12 | JPS5968020A | 1984-04-17 | MIHARA SOUICHIROU |
| PURPOSE:To obtain an autopilot of a flying object which eliminates the need for high-precision acceleration and an electric interface with a mother equipment and utilize a special Pitot static pressure tube, by varying the gain of an autopilot according to operation altitude and a speed. CONSTITUTION:The output of the Pitot static pressure tube 16 provided to the autopilot is converted into electric signals by total pressure and static pressure gauges 29 and 30, and a strain gauge 22 measures air force operating on plural small blades fitted to the Pitot static pressure tube. This air force is transduced into voltages by dynamic strain gauges 27 and 28 for a pitch axis and total pressure, and altitude and speed computers 33 and 34 find the altitude and speed from the difference between the total pressure and static pressure. Further, the outputs of the dynamic strain gauges 27 and 28 are converted into estimated acceleration by acceleration computers 31 and 32 which calculate pitch-axis and yaw-axis acceleration. Then, the pitch-axis and yaw-axis rate gyros 1 and 5 detects the angular speed of the frame body and the gain of the autopilot is adjusted by a gain adjusting device 13 according to the altitude and speed information. | ||||||
| 256 | Vehicular autopilot | JP30903699 | 1999-10-29 | JP2001122145A | 2001-05-08 | HATANO TSUTOMU |
| PROBLEM TO BE SOLVED: To prevent an autopilot from being stopped by an unintended steering wheel operation. SOLUTION: A steering shaft 1 and an output shaft 3 are collinearly connected via gears 6 and 8 and a planetary gear 7. A lane detecting device 11 detects a lane whereon a vehicle is traveling, and this lane information is outputted to an automatic steering controller 10 along with a vehicular state signal from a control system of the vehicle. In the automatic steering controller, when it is determined from the lane information that the vehicle has drifted from the lane, a steering control motor 19 is controlled so as to correct this drift. Meanwhile, when a steering wheel is operated and the output shaft is rotated in an opposite direction, the automatic steering is stopped. For a steering torque during the automatic steering, when an electrical apparatus is operated, a first steering torque is used, and when it is not, a second steering torque is used. The second steering torque is set larger than the first steering torque for preventing automatic steering mode from being canceled by an unintended steering wheel operation when operating the electrical apparatus. | ||||||
| 257 | Servoamplifier for marine auto pilot | JP32791787 | 1987-12-24 | JPH01168594A | 1989-07-04 | ASHI MICHIAKI |
| PURPOSE: To make accuracy in a system maintainable as a whole to a power source variation by constituting a sampling timing circuit so as to make a displacement value to the power source variation of a sampling point smaller to the utmost. CONSTITUTION: A servoamplifier supply voltage is rectified by a pair of rectifying devices D 1, D 2, clipped by a par of clipping elements Z 1, Z 2, and wave shaping is carried by wave shaping circuits (R 1, R 2) and (Q 1, Q 2), thereby generating a first switching control signal and a second switching control signal, and each startup of these control signals is set to the voltage set by the clipping elements Z 1, Z 2, whereby the startup is set to a very near position after zero point passage of a voltage waveform and thereby variations in each startup waveform position of these control signals is made to be little to a supply voltage variation. A pair of switching elements SW 1, SW 2 are synchronized with an actual steering angle signal by these control signals and turned on or off alternately, outputting it to a smoothing circuit 40c and, after being smoothed hereat, it is amplified by an amplifier 40e, thereby outputting it as a DC voltage proportioned to a sine. COPYRIGHT: (C)1989,JPO&Japio | ||||||
| 258 | Motor-driven auto-adjuster | JP9700979 | 1979-07-30 | JPS5620842A | 1981-02-26 | OGAWA YUTAKA |
| PURPOSE: To adjust the clearance to a proper value by an auto-adjuster when the clearance has increased due to the wear of the lining of a drum brake. CONSTITUTION: When the wear of the linings 1a, 1a' of brake shoes 1, 1' has exceeded a predetermined value, a motor (which is located behind a worm gear 10) extends an adjusting screw 7 integral with a screw gear 7c in relation to a strut nut 5 so as to once nullify the shoe clearance when the operating switch for a control circuit is turned on. Then, according to a program, the motor is rotated reversely by a predetermined number of turns to obtain a preset shoe clearance. The overadjustment due to the thermal expansion of the drum can be prevented by incorporating a brake temperature detecting circuit, for example, including a thermistor, into the motor controlling circuit. COPYRIGHT: (C)1981,JPO&Japio | ||||||
| 259 | Autopilot navigation | US14693753 | 2015-04-22 | US09545988B2 | 2017-01-17 | Jeremiah Clark |
| Various implementations described herein are directed to a non-transitory computer-readable medium having stored thereon a plurality of computer-executable instructions which, when executed by a computer, cause the computer to: receive a range of headings at a marine electronics device and analyze sonar data received from a sonar device coupled to a vessel to determine a first characteristic measured at a first location. The first characteristic may be a bottom hardness, a bottom composition, a transition between bottom compositions, a water temperature, or a thermocline. The instructions may further cause the computer to: compare the first characteristic to a second characteristic measured at a second location and transmit instructions to an autopilot to move the vessel in a heading in the range of headings. The instructions are based at least in part on the comparison between the first characteristic and the second characteristic. | ||||||
| 260 | Trolling autopilot | US858097 | 1992-03-26 | US5362263A | 1994-11-08 | Ralph E. Petty |
| An autopilot for a vessel for use in combination with a depth finder having a transducer, including a means for setting and storing a desired characteristic to be followed by the vessel, means for measuring the characteristic to be followed by the vessel, and means for storing a signal generated by the measuring means indicative of the measured characteristic. Once received and stored, the measured characteristic is compared to the selected characteristic. Based upon the comparison between the two characteristics, at least one servo motor is actuated to alter the direction the vessel is traveling. A servo motor may be coupled to the helm or to an outboard motor mounted to the vessel. The speed of the vessel may also be controlled based upon a comparison between a measured value and a selected value. | ||||||
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