| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 321 | Light Guided autopilot | US09717770 | 2000-11-21 | US06456910B1 | 2002-09-24 | John Andrew Roe |
| An autopilot system for a vehicle capable of steering the vehicle on a predetermined course by use of laser beams. The invention is comprised of: an off-board mounted laser transmitter, which describes the intended course of the vehicle, a vehicle mounted laser sensor array, a logic control unit, one or more actuators to control vehicle's heading and a user interface. | ||||||
| 322 | Pedestal mount autopilot | US251464 | 1981-04-06 | US4392446A | 1983-07-12 | Gerardus H. Vander Eyken; James J. Thoman |
| A self contained electro-mechanical arrangement for use in autopilot for yachts for securement to a steering wheel pedestal column is disclosed. The arrangement comprises a magnetic directional indicator, sensing apparatus associated with the magnetic directional indicator for determining movement thereof, and electrical drive controlled by the sensing apparatus. The electrical drive includes an electric motor, and a transmission, with the electric motor being bi-directional to allow rotation of the output shaft of the transmission in either direction. A mechanical drive is associated with the transmission for engaging the steering wheel shaft of such yacht wherein the motor and the directional indicator are separated to reduce any effect of the motor on the movement of the magnetic directional indicator. | ||||||
| 323 | Torpedo autopilot servo | US25897563 | 1963-02-14 | US3167048A | 1965-01-26 | RAMSTEDT CLARENCE F |
| 324 | Control assembly for automatic pilot | US72840958 | 1958-04-14 | US3080877A | 1963-03-12 | HUNT ELWOOD M |
| 325 | Autopilot simulator | US80792059 | 1959-04-21 | US3000112A | 1961-09-19 | CRABB MERLE W |
| 326 | Compass suspension for automatic pilot | US85277459 | 1959-11-13 | US2973413A | 1961-02-28 | HILL ARTHUR D |
| 327 | Autopilot steering system | US18761350 | 1950-09-29 | US2866146A | 1958-12-23 | RODRIGUEZ JR CHARLES F |
| 328 | Maneuverable automatic pilot for ships | US33011253 | 1953-01-07 | US2796576A | 1957-06-18 | BRADDON FREDERICK D; WEST JR FRANCIS |
| 329 | 비접촉 매체를 이용한 다중 코드 생성 방식의 오티피 운영 방법 | KR1020170091767 | 2017-07-19 | KR1020170088320A | 2017-08-01 | 김재형; 권봉기 |
| 본발명의비접촉매체를이용한다중코드생성방식의오티피운영방법에따르면, OTP(One Time Password)를구현하는프로그램을설치한사용자휴대폰과통신하는서버를통해실행되는방법에있어서, 상기프로그램을설치구동한사용자휴대폰을사용자의 OTP를구현하는사용자의 OTP 매체로인증받기위해상기사용자휴대폰에상기프로그램이다운로드설치된후 별도로중복되지않게고유할당되어상기사용자휴대폰의지정된저장영역에저장되는식별자를등록받아지정된저장매체에저장하는절차와상기사용자휴대폰에상기프로그램이설치되기전부터상기사용자휴대폰을식별하기위해기 할당된전화번호나일련번호중 적어도하나의번호정보를등록받아상기저장매체에저장하는절차를수행하고상기사용자휴대폰의매체리더부를통해사용자가별도로소유한비접촉매체로부터리딩될코드정보를인증하기위한정보를지정된저장매체에저장시키는절차를수행하고, 상기번호정보에대응하는사용자휴대폰에서상기프로그램이구동되면, 상기사용자휴대폰에서구동된프로그램으로부터상기사용자휴대폰의지정된저장영역으로부터추출되어전송된식별자를수신하고상기저장매체에저장된식별자와비교인증하여상기프로그램을설치구동한사용자휴대폰을상기사용자의 OTP 매체로인증하는절차를수행하고상기사용자휴대폰의매체리더부를통해상기비접촉매체로부터리딩된코드정보를수신하여상기저장매체에저장된코드정보를통해비교인증하는절차를수행하고, 상기식별자를통해상기프로그램을구동한사용자휴대폰을사용자의 OTP 매체로인증하고상기코드정보를통해사용자가상기 OTP 매체외에별도의비접촉매체를소유함을인증한경우, 상기사용자휴대폰측에서생성되어상기휴대폰의프로그램을통해전송된단말측 코드값을확인하고서버측에서결정된서버측 생성정보를확인한후 상기단말측 코드값과상기서버측 생성정보를이용하여사용자휴대폰의프로그램을통해 N(N≥2)자리수의 OTP를생성하기위한생성정보를구성하며, 상기인증된 OTP 매체에대응하는사용자휴대폰의프로그램으로상기생성정보를제공한다. | ||||||
| 330 | 곡물 공급 조절기구를 갖는 제분용 롤밀의 자동 조절장치 | KR1019810001223 | 1981-04-10 | KR1019830004885A | 1983-07-20 | 베르너빈텔러; 로베르트린즈베르거; 렌데르트케팅; 한스외티커 |
| 내용없음 | ||||||
| 331 | OPERATOR SKILL SCORING BASED ON COMPARISON TO AUTOMATED VEHICLE OPERATION | PCT/US2016/066857 | 2016-12-15 | WO2017131886A1 | 2017-08-03 | WIESKAMP, Jonathan, L.; HILNBRAND, Brian, R.; PENDELTON, Nathan, A.; MANGAL, Nandita |
A skill-scoring system (10) suitable for use on an automated vehicle (12) includes an accelerometer (22) and a controller (20). The accelerometer (22) is used to determine an acceleration-value (24) experienced by an operator (16) of a host-vehicle (12) while the operator (16) operates the host-vehicle (12) in a manual-mode (14) along a travel-path (26). The controller (20) is in communication with the accelerometer (22). The controller (20) is configured to determine a skill-score (32) based on a comparison of the acceleration- value (24) to an expected-acceleration (34) that the operator (16) would experience when the host-vehicle (12) is operated in an automated-mode (18) along the travel-path (26). |
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| 332 | AUTOMATE DONNANT LA POSSIBILITE DE SE BROSSER LES DENTS DANS UN LIEU PUBLIC | PCT/FR2006/000585 | 2006-03-16 | WO2006103328A1 | 2006-10-05 | HOUARI, Kaddour, Karim; HOUARI, Samir |
Automate donnant la possibilité de se brosser les dents avec une brosse à dents électrique dans les lieux publics. Le domaine technique de l'invention se situe dans celui des distributeurs automatiques. Il comprend un compartiment autonettoyant (1) dans lequel se situe un corps de brosse électrique (6) ; une ouverture de réception (2) qui distribue le matériel nécessaire au brossage des dents. Aucun automate ne permet de se brosser les dents dans un lieu public. La solution technique est apportée par notre automate dans la mesure où il donne la possibilité de se brosser les dents dans un lieu public. Pour le fonctionnement de l'appareil, l'introduction de monnaie par le biais du monnayeur (9) est nécessaire. Par la suite en appuyant sur le bouton de mise en marche (J), la porte étanche (8) s'ouvre, le gobelet (3) chute dans l'ouverture prévue à cet effet, suivi de la « brossette » (5) et de la « dosette » (4) de dentifrice qui tombent dans le gobelet. L'utilisateur n'a plus qu'à se saisir du corps de brosse électrique (5) auquel il ajoute la brossette. Il peut donc maintenant se brosser les dents avec le dentifrice fourni. L'automate selon l'invention est particulièrement destiné aux restaurants. |
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| 333 | HELICOPTER AUTOPILOT PROVIDING AIRSPEED CONTROL | PCT/FR1995000033 | 1995-01-11 | WO1995019592A1 | 1995-07-20 | |
| A novel basic architecture for helicopter autopilots where the conventional fuselage attitude control function is turned into an airspeed control function without resorting to coupler technology. A known fraction of the flight control output signal (24S) is added to a standard fuselage attitude input (1S) and fed to each of the two pitch and roll channels, and the resulting signal (4S) has the new static and dynamic properties needed for the control loop to impart static speed stability to the helicopter throughout the flight envelope. Said novel architecture enables the conventional fuselage attitude signal (1S) to be replaced with an accelerometer signal. By displaying the signal (4S), in particular on a standard attitude indicator instrument (33), rapid changes in fuselage attitudes may be monitored and airspeeds may at the same time be controlled. | ||||||
| 334 | Device carrier and horizontal transfer, type autohandler | JP9423699 | 1999-03-31 | JP2000292487A | 2000-10-20 | KUNINOBU SEIJI; UCHINO YOSHIAKI |
| PROBLEM TO BE SOLVED: To stably measure an electric characteristic of a device such as an IC or the like by surely connecting a terminal of the device to the contact element of a socket. SOLUTION: A recess 11a where an IC 1 is to be arranged is formed to a device carrier 11 disposed above an IC socket 2. Positioning hole parts 13 are formed to a positioning plate part 12 constituting a bottom part of the recess 11a, to which solder balls 1a of the IC 1 arranged in the recess 11a are fitted. When the device carrier 11 holding the IC 1 is placed above the IC socket 2, contact elements 2a of the IC socket 2 are inserted and positioned to the positioning hole parts 13, so that the contact elements 2a and the solder balls 1a of the IC 1 can be surely brought in contact with each other. COPYRIGHT: (C)2000,JPO | ||||||
| 335 | Suction mechanism for ic and horizontal carry type autohandler | JP29103598 | 1998-10-13 | JP2000117676A | 2000-04-25 | TANAKA HIDEYUKI; OKAMOTO KAZUMI |
| PROBLEM TO BE SOLVED: To eliminate a problem such as a misidentifying, caused by suction of a tray with a suction pad, to enable detection of the presence or absence of an IC on the tray, and to improve the availability of a horizontal carry type autohandler by applying a suction mechanism of the IC. SOLUTION: A stopper 6F having a step part 61 projecting downward so as to cover a suction pad 6A is attached to a lower end of a shaft 6B. A suction hand is descended, and then if an IC5 does not exist on a recessed part 4a of the tray 4, the stopper 6F abuts on an upper surface 41 of the tray 4 and the suction pad keeps spacing with a bottom surface 4b of the tray 4. A pressure sensor is provided on an extending part of the shaft 6B, and the presence or absence of the IC 5 on the tray 4 is detected by the degree of a negative pressure of the pressure sensor. | ||||||
| 336 | Roll baler traveling autostopper | JP35359393 | 1993-12-27 | JPH07184459A | 1995-07-25 | YAMANAKA TAKESHI |
| PURPOSE: To provide a roll baler traveling autostopper designed to obviate working mistakes by omitting manual operations and improve working efficiency by shortening working time. CONSTITUTION: In an autostopping system so designed as to be equipped with a bale-making chamber, a binder to wrap bales with strings and a delivery mechanism to draw out bales after bound, it is so constituted that a traveling clutch is switched to 'off' subsequently to the 'on' operation of a working clutch lever 5 actuating the string feeding mechanism in the binder on completing a bale in the bale-making chamber. COPYRIGHT: (C)1995,JPO | ||||||
| 337 | Carriage automatic driver of hand knitting machine | JP20105484 | 1984-09-25 | JPS6183361A | 1986-04-26 | KAWAI MASATOSHI; ITO MASAO |
| 338 | Method of controlling autowiper for car | JP10416984 | 1984-05-23 | JPS60248458A | 1985-12-09 | MUTOU MASAHITO |
| PURPOSE:To obtain a natural wiping operation of a wiper by reducing a detecting time cycle for a stop control mode, when a wiper control mode is discontinuously switched from an operation control mode for dealing with a quantity of rain above a certain value, to said stop control mode. CONSTITUTION:A program for controlling wiper is previously set in a ROM24, and a CPU26 controls the operation of each part according to the program. When a wiper control mode is discontinuously switched from an Hi mode to a stop control mode without passing through an L0 mode or an Int mode, e.g., when a car entered a tunnel, an Hi flag is continuously set at on, a defined bias is applied to a timer to reduce the detecting time cycle for the stop control mode, a short cycle for waiting an Hi mode operation is set, and carry out a wiper control for rapidly detecting the quantity of rain when traveling in rain is resumed, obtaining a good front vision. | ||||||
| 339 | AUTOPILOT SIMULATION SYSTEM AND METHOD | PCT/US2012051878 | 2012-08-22 | WO2013032812A3 | 2013-04-25 | MILLER LOUIS EDWARD |
| A computer implemented method is described. A computer-implemented method provides determining if an extended absence flag has been triggered for a first participant. If the extended absence flag has been triggered, the computer-implemented method automatically performs one or more of a plurality of actions required to continue game play on behalf of the first participant as if the first participant was still actively involved in game play. By automatically conducting play of the first participant as if the first participant was still involved, the computer-implemented method maintains competitiveness as well as the game experience for other participants. | ||||||
| 340 | VISUAL AUTOPILOT FOR NEAR-OBSTACLE FLIGHT | PCT/IB2008/051497 | 2008-04-18 | WO2009127907A1 | 2009-10-22 | ZUFFEREY, Jean-Christophe; BEYELER, Antoine; FLOREANO, Dario |
This present invention describes a novel vision-based control strategy for autonomous cruise flight in possibly cluttered environments such as - but not limited to - cities, forests, valleys, or mountains. The present invention is to provide an autopilot that relies exclusively on visual and gyroscopic information, with no requirement for explicit state estimation nor additional stabilisation mechanisms. This approach is based on a method of controlling an aircraft having a longitudinal axis comprising the steps of: a) defining at least three viewing directions spread within frontal visual field of view, b) acquiring rotation rates of the aircraft by rotation detection means, c) acquiring visual data in at least said viewing directions by at least one imaging device, d) determining translation-induced optic flow in said viewing directions based on the rotation rates and the visual data, e) estimating the proximity of obstacles in said viewing directions based on at least the translation-induced optic flow, f) for each controlled axes (pitch, roll and/or yaw), defining for each proximity, a conversion function to produce a converted proximity related to said controlled axe, g) determining a control signal for each controlled axes by combining the corresponding converted proximities, h) using said control signals to drive the controlled axes of the aircraft. |
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