序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
161 ABSOLUTE ACCELERATION SENSOR FOR USE WITHIN MOVING VEHICLES EP07839779.1 2007-10-23 EP2084598A2 2009-08-05 BRAUNBERGER, Alfred S.; BRAUNBERGER, Beau M.
A communication system for a vehicle includes a vehicle speed sensor configured to emit a periodic function with a parameter correlated to the speed of the vehicle, an acceleration monitoring system, a braking system engagement detector to detect a braking status of the vehicle, an alerting device capable of signaling other drivers of a deceleration condition of the vehicle, and a control device. The acceleration monitoring system is configured to compute the acceleration of the vehicle from variations in the parameter of the periodic function of the vehicle speed sensor and to output a deceleration status of the vehicle. The control device is coupled to the acceleration monitoring system, the braking system engagement detector, and the alerting device, wherein the acceleration monitoring system sends signals to the control device and the control device operates the alerting device in a manner dependent on the deceleration status of the vehicle.
162 Dual mode mems sensor EP07119630.7 2007-10-30 EP1918723A3 2008-06-25 Platt, William P.; Henrickson, Jens

A system and method for determining acceleration along a motor axis of a MEMS gyroscope includes a processor. The processor includes a notch filter to remove a sinusoid from an instantaneous voltage from a motor pick up of the MEMS gyroscope. A memory bus allows random access to data stored in a processor readable memory. A processor-readable memory in operative engagement with the memory bus allows access to the processor-readable memory containing data. The data includes a model relating at least one instantaneous voltage in a remaining instantaneous voltage to an acceleration of a proof mass along the motor axis. Instructions to the processor include a routine to compare the at least one instantaneous voltage in the model to the remaining instantaneous voltage.

163 Combined sensor and its fabrication method EP06018553.5 2006-09-05 EP1762823A2 2007-03-14 Akashi, Teruhisa, c/o Hitachi, Ltd.; Okada, Ryoji, c/o Hitachi, Ltd.; Hayashi, Masahide, c/o Hitachi, Ltd.; Suzuki, Kengo, c/o Hitachi, Ltd.

A sensor structure using vibrating sensor elements (1a, 1b, 1c, 1d) which can detect an angular rate and accelerations in two axes at the same time is provided. 2 sets of vibration units (1a, 1b; 1c, 1d) which vibrate in out-of-phase mode (tunning-fork vibration) and include four vibrating sensor elements of the approximately same shape supported on a substrate in a vibratile state are provided and the vibrating sensor elements are disposed so that vibration axes of the vibration units cross each other at right angles. Each of the vibrating sensor elements includes a pair of detection units (3a, 3b, 3c, 3d) and adjustment units (4a, 4b, 4c, 4d) for adjusting a vibration frequency. The vibrating sensor elements constitute a combined sensor having supporting structure for supporting the vibrating sensor elements independently so that the vibrating sensor elements do not interfere with each other.

164 MICRO-MACHINED MULTI-SENSOR PROVIDING 1-AXIS OF ACCELERATION SENSING AND 2-AXES OF ANGULAR RATE SENSING EP04750818.9 2004-04-27 EP1618392A2 2006-01-25 GEEN, John, A.
A micro-machined multi-sensor that provides 1-axis of acceleration sensing and 2-axes of angular rate sensing. The multi-sensor includes a plurality of accelerometers, each including a mass anchored to and suspended over a substrate by a plurality of flexures. Each accelerometer further includes acceleration sense electrode structures disposed along lateral and longitudinal axes of the respective mass. The multi-sensor includes a fork member coupling the masses to allow relative antiphase movement, and to resist in phase movement, of the masses, and a drive electrode structure for rotationally vibrating the masses in antiphase. The multi-sensor provides electrically independent acceleration sense signals along the lateral and longitudinal axes of the respective masses, which are added and/or subtracted to obtain 1-axis of acceleration sensing and 2-axes of angular rate sensing.
165 SILICON MACROMACHINED SYMMETRIC VIBRATORY GYROSCOPE SENSOR EP97928679.6 1997-05-30 EP0902875B1 2004-11-24 TANG, Tony, K.; KAISER, William, J.; BARTMAN, Randall, K.; WILCOX, Jaroslava, Z.; GUTIERREZ, Roman, C.; CALVET, Robert, J.
A microgyroscope (10) comprising a silicon, four-leaf clover structure (12) which is suspended by four silicon cantilevers or springs (14) extending between clover (12) and rim (16). The device is electrostatically actuated and capacitively detects Coriolis induced motions of the leaves of the clover leaf structure. In a preferred embodiment, a post (18) is attached through a center (20) of the clover structure (12) in a direction symmetrically perpendicular to both sides of a plane formed by the clover leaves (22a-b). In the case where the post is not symmetric with the plane of the clover structure, the device is usable as an accelerometer. If the post is provided in the shape of a dumb bell or an asymmetric post, the center of gravity is moved out of the plane of the clover leaf structure and a hybrid device is provided. When the clover leaf structure is used without a center mass, it performs as a high Q resonator usable as a sensor of any physical phenomena.
166 ACCELERATION DETECTION TYPE GYRO DEVICE EP01906216.5 2001-02-22 EP1275934A1 2003-01-15 KARASAWA, Satoshi Tokimec Inc.; MURAKOSHI, Takao Tokimec Inc.; FUKATSU, Keisuke Tokimec Inc.

An acceleration-detecting type gyro apparatus of an electrostatic supporting type, in which displacements of a gyro rotor are actively made zero is proposed. The acceleration-detecting type gyro apparatus includes: a gyro case; a gyro rotor which is supported within the gyro case by electrostatic supporting forces such that the gyro rotor is not in contact with the gyro case; electrostatic supporting electrodes for generating the electrostatic supporting forces; a rotor drive system for rotating the gyro rotor around the spin axis at high speed; a displacement-detection system for detecting displacements of the gyro rotor; and a restraining system having a feedback loop for correcting control voltages applied to the electrostatic supporting electrodes so that displacements of the gyro rotor become zero, the gyro rotor is annular-shaped, and the electrostatic supporting electrodes are disposed in a manner of surrounding the gyro rotor.

167 PENDULOUS OSCILLATING GYROSCOPIC ACCELEROMETER EP95929386 1995-08-04 EP0784797A4 1997-12-17 SAPUPPO MICHELE S
A pendulous oscillating gyroscopic accelerometer (10) comprising an unbalanced pendulous mass (28), pivotable on an output axis, that is oscillated about a reference axis transverse to the output axis. The pendulous mass (28) is also oscillated about an input axis transverse to the reference axis using a control servo loop (40), and the acceleration force along the input axis is determined from at least one of those oscillations.
168 VORRICHTUNG UND VERFAHREN ZUR GLEICHZEITIGEN MESSUNG EINER DREHRATE UND EINER TRANSVERSALEN BESCHLEUNIGUNG EP95930398.0 1995-09-15 EP0786073A1 1997-07-30 ROTHLEY, Manfred; ZABLER, Erich; WOLF, Jörg
The proposal is for a device and a process for the simultaneous determination of a rate of rotation W and an acceleration atr transverse to the axis of rotation. Said device has at least one acceleration sensor (1, 2) on each of at least two sections (3, 4) fitted in such a way that its axis (Z1, Z2) sensitive to accelerations (ac1, ac2, atr) does not lie in the plane formed by the axis of rotation (D) and the velocity component (v) of the oscillation. In implementing the process, the device is rotated about the axis (D) at a rotation speed corresponding to the speed W to be determined, and simultaneously the device is caused to oscillate at at least two sections (3, 4) with a velocity component (v1, v2) perpendicular to the axis of rotation (D). With the symmetrical fitting of identical acceleration sensors (1, 2) to the device, the rate of rotation W and the transverse acceleration atr can be obtained in a simple manner by adding or substracting the measurement signals detected in the acceleration sensors (1, 2).
169 Capteur inertiel composite du type mécanique EP89400678.2 1989-03-10 EP0336795B1 1991-09-11 Martin, Frédéric
170 Capteur inertiel composite du type mécanique EP89400678.2 1989-03-10 EP0336795A1 1989-10-11 Martin, Frédéric

Capteur inertiel composite du type mécanique. Le rotor (1) et l'arbre d'entraînement (5) sont mécanique­ment reliés par une jante souple (3), déformable élasti­quement et agencée pour laisser au susdit rotor (1) trois degrés de liberté, à savoir un degré de liberté en translation selon l'axe de rotation arbre d'entraînement (5)-rotor (1), et deux degrés de liberté en rotation autour de deux axes formant un trièdre avec ledit axe de rotation. Un dispositif à moteurs couples (6) est prévu pour exercer sur le susdit rotor (1) au moins trois forces parallèles au susdit axe de rotation, et un dis­positif détecteur (7) est prévu pour déterminer la position du susdit rotor (1) par rapport à la structure du capteur.

171 COMPUTING SYSTEM IMPLEMENTING AN ALGORITHM FOR FUSING DATA FROM INERTIAL SENSORS, AND METHOD EP18172853.6 2018-05-17 EP3407157A1 2018-11-28 ZANCANATO, Alberto; FERRAINA, Michele; RIZZARDINI, Federico; RIVOLTA, Stefano Paolo

A computing system (10) including: a first hardware element (12, 14), housing a first accelerometer (20; 22) and a first gyroscope (24; 26); a second hardware element (14; 12), housing a second accelerometer (22; 20) and a second gyroscope (26; 24), which can be oriented with respect to the first hardware element (12) and defines an angle (αLID) with the first hardware element (12; 14); and a calculating unit (27, 28) configured for performing the operations of: calculating a first intermediate value (αLID_ACC) of the angle (αLID) on the basis of signals generated by the first and by the second accelerometers (20, 22); calculating a second intermediate value (αLID_GYR) of the angle (αLID) on the basis of signals generated by the first and by the second gyroscopes (24, 26); calculating a final value of the angle (αLID) as the weighted sum of the first intermediate value (αLID_ACC) and of the second intermediate value (αLID_GYR) ; and controlling at least one parameter of the computing system (10) as a function of the final value of the angle (αLID).

172 CONTROL METHOD FOR DIGITAL SIGHT EP14905474.4 2014-11-13 EP3217140B1 2018-10-31 LEE, Tae-Gyoo; JANG, Suk-Won; LEE, Jin Seung; CHOI, Jae-Gun; MOON, Hong-Key
The present invention relates to a digital sight for a hand-carried projectile-firing device and a method of controlling the digital sight. A digital sight for a hand-carried projectile-firing device according to an embodiment of the present invention is a digital sight (100) for a hand-carried projectile-firing device, the digital sight (100) including an inertial sensor package (200) and a manual rotation device (300), wherein the inertial sensor package (200) includes a gyroscope (210) and an accelerometer module (220). In accordance with the present invention, equipment for measuring the firing direction of a hand-carried projectile-firing device such as a mortar is replaced with a digital sight for a hand-carried projectile-firing device, which reduces an estimation error while using a single medium-low level gyroscope, thus enabling the projectile-firing device to precisely and promptly fire a projectile and improving the operability thereof.
173 MOTION SENSING FOR AN AEROSOL DELIVERY DEVICE EP16813034.2 2016-12-06 EP3386324A1 2018-10-17 SUR, Rajesh; SEARS, Stephen B.
An aerosol delivery device includes at least one housing; and contained within the at least one housing, a control component and motion sensor. The control component may control operation of the aerosol delivery device based on a detected flow of air through at least a portion of the at least one housing. The motion sensor may detect a defined motion of the aerosol delivery device that indicates a vulnerability of the aerosol delivery device or a user thereof, with the motion sensor being configured to convert the defined motion to an electrical signal. The control component or motion sensor may recognize the vulnerability and an operation associated with the vulnerability based on the electrical signal, and the control component may control at least one functional element of the aerosol delivery device to perform the operation, which may thereby be performed in response to detection of the vulnerability.
174 MULTIAXIAL MICRO-ELECTRONIC INERTIAL SENSOR EP12821255.2 2012-12-20 EP2795253B1 2018-10-03 LECLERC, Jacques
A resonator micro-electronic inertial sensor, preferably a micro-electromechanical system (MEMS) sensor (e.g. a gyro), for detecting linear accelerations and rotation rates in more than one axis comprises: €¢ a proof-mass system (21.1, ..., 21.4) flexibly suspended above a substrate for performing a rotational in-plane vibration about a central axis (24,) €¢ a drive electrode system (D1, ..., D4) for driving the proof-mass system (21.1, ..., 21.4) to perform said rotational in-plane vibration, €¢ and a sensing electrode system (S1, ..., S8) connected to the proof-mass system (21.1, ..., 21.4) for detecting linear accelerations or rotation rates in more than one axis. Said proof-mass system (21.1, ..., 21.4) has more than two proof-mass elements flexibly coupled (25.1a, 25.1 b) to each other. Each proof-mass element (21.1, 21.2) is directly and flexibly connected (23.1, 25.1a, 25.1 b) to an anchor structure (22) on the substrate (32). The proof-mass elements (21.1, ..., 21.4) are preferably arranged in a ring-shaped configuration between an inner and an outer radius (R1, R2) with respect to the central axis (24).
175 Disc resonator integral inertial measurement unit. EP08075661.2 2008-07-25 EP2028440B1 2018-09-05 Challoner, A. Dorian; Whelan, David
Sensing motion of multiple degrees of freedom for an integral inertial measurement unit provided through the operation of a single centrally mounted planar disc resonator having a single driven mode in a single vacuum enclosure is disclosed. The resonator comprises a circumferentially slotted disc having multiple internal capacitive electrodes within the slots in order to excite a single in-plane driven vibration and sense in-plane vibration modes or motion of the resonator. In addition, vertical electrodes disposed below and/or above the resonator may also be used to sense out-of-plane vibration or motion. Acceleration sensing in three orthogonal axes can be obtained by sensing two lateral modes of the disc resonator in the plane of the disc from the internal electrodes and a vertical mode from the vertical electrodes.
176 VESTIBULAR IMPLANT COMPRISING A HYBRID MEMS MICROFLUIDIC GYROSCOPE EP13812069.6 2013-09-04 EP2893296B1 2018-08-29 Georgiou, Julius; Andreou, Charalambos, Micheal
A hybrid MEMS microfluidic gyroscope is disclosed. The hybrid MEMS microfluidic gyroscope may include a micro-machined base enclosure having a top fluid enclosure, a fluid sensing enclosure and a bottom fluid enclosure. The hybrid MEMS microfluidic gyroscope may include a plurality of cantilevers disposed within the bottom semi-circular portion of the micro-machined base enclosure or a single membrane disposed within the bottom semi-circular portion of the micro-machined base enclosure.
177 METHOD AND DEVICE FOR BLURRING A VIRTUAL OBJECT IN A VIDEO EP16306175.7 2016-09-15 EP3296950A1 2018-03-21 JOUET, Pierrick; ROBERT, Philippe; FRADET, Matthieu

In order to blur a virtual object in a video in real time as the video is acquired by a device capturing a real scene, a salient idea comprises estimating an apparent motion vector between two successive images, being captured at two successive device poses, wherein the apparent motion vector estimation is based on a motion of the device. The successive images are then filtered based on the estimated apparent motion vector.

178 DYNAMIC FORCE SENSING TO DETERMINE MASS USING A SMARTPHONE EP14745280.9 2014-07-03 EP3028016B1 2017-08-30 TCHERTKOV, Igor; PARLAK POLATKAN, Siddika
179 VEHICLE MONITORING MODULE EP15731770.2 2015-06-03 EP3152520A1 2017-04-12 GREER, Dale, R.
A portable system for monitoring vehicle driving conditions is provided. The system may include a processor, an accelerometer unit, and a gyroscope unit. The processor may be configured to determine a primary axis of the vehicle based on acceleration data from the accelerometer unit and the angular rate of change data from the gyroscope unit.
180 An integrated global navigation satellite system and inertial navigation system EP13153646.8 2013-02-01 EP2762834B1 2017-03-22 Mertens, Christophe
QQ群二维码
意见反馈