子分类：
- G01S7/4802： ..{利用用于表明目标特性的回波信号的分析;目标形状;目标截面}
- G01S7/4804： ..{ 用于检测或识别激光雷达信号或类似物的辅助装置,例如激光照明装置}
- G01S7/4808： ..{距离、位置或速度数据的估计}
- G01S7/481： ..结构特征,例如光学元件的布置
- G01S7/483： ..脉冲系统的零部件
- G01S7/491： ..非脉冲系统的零部件
- G01S7/495： ..对抗或反对抗测量{使用电子的或电光装置}
- G01S7/497： ..监测或校准装置
- G01S7/499： ..使用极化效应(光的极化测量入G01J)
- G01S7/51： ..显示装置
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 201 | Accident avoidance system | US09679317 | 2000-10-04 | US06405132B1 | 2002-06-11 | David S. Breed; Wendell C. Johnson; Wilbur E. Duvall |
| System and method for preventing vehicle accidents in which GPS ranging signals relating to a host vehicle's position on a roadway on a surface of the earth are received on a first communication link from a network of satellites and DGPS auxiliary range correction signals for correcting propagation delay errors in the GPS ranging signals are received on a second communication link from a station or satellite. The host vehicle's position on a roadway on a surface of the earth is determined from the GPS, DGPS, and accurate map database signals with centimeter accuracy and communicated to other vehicles. The host vehicle receives position information from other vehicles and determines whether any other vehicle from which position information is received represents a collision threat to the host vehicle based on the position of the other vehicle relative to the roadway and the host vehicle. If so, a warning or vehicle control signal response to control the host vehicle's motion is generated to prevent a collision with the other vehicle. | ||||||
| 202 | Airbag inflation control system and method | US09825173 | 2001-04-03 | US20020027339A1 | 2002-03-07 | David S. Breed |
| Airbag inflation control system and method for a vehicle including an airbag module having a housing mounted in combination with the seat back and an inflatable airbag arranged therein. An anticipatory sensor detects that an impact requiring deployment of the airbag is required based on data obtained prior to the crash and initiates inflation of the airbag in the event an impact requiring deployment of the airbag is detected prior to the start of the impact. An inflator responds to the detection by the anticipatory sensor that an impact requiring deployment of the airbag is required and inflates the airbag. The occupant may be displaced upon inflation of the airbag. | ||||||
| 203 | Vehicular component control systems and methods | US09838919 | 2001-04-20 | US20010029416A1 | 2001-10-11 | David S. Breed; Wilbur E. DuVall; Wendell C. Johnson |
| System and method for controlling operation of a vehicle or a component thereof based on recognition of a individual including a processor embodying a pattern recognition algorithm trained to identify whether a person is the individual by analyzing data derived from optical images and an optical receiving unit for receiving images including the person and deriving data from the images. The optical receiving unit provides the data to the algorithm to obtain an indication from the algorithm whether the person is the individual. A security system enables operation of the vehicle when the algorithm provides an indication that the person is an individual authorized to operate the vehicle and prevents operation of the vehicle when the algorithm does not provide an indication that the person is an individual authorized to operate the vehicle. A component adjustment system adjusts the component based on the recognition of the individual. | ||||||
| 204 | Side impact airbag systems | US09024085 | 1998-02-17 | US06209909B1 | 2001-04-03 | David S. Breed |
| A variable inflation rate inflator system for inflating one or more airbags including an inflator for releasing a gas into the airbag(s), a first anticipatory crash sensor for determining that a crash requiring an airbag will occur based on data obtained prior to the crash and, upon the making of such a determination, triggering the inflator means to release gas into the airbag(s) to thereby inflate the same at a first inflation rate, and a second crash sensor for determining that a crash requiring an airbag will occur or is occurring and, upon the making of such a determination, affecting the inflator such that an additional quantity of gas is released thereby into the airbag(s) to thereby inflate the airbag(s) at a second inflation rate greater than the first inflation rate. Also, an airbag passive restraint system for protecting an occupant sitting in the seat adjacent the side door is disclosed including at least one airbag arranged to be inflated between the occupant and the side door, a sensor for detecting that a crash requiring deployment of the airbag(s) is required, an inflator for releasing a gas into the airbag(s) to inflate the same and which is triggered by the sensor to release gas into the airbag(s) in response to the detection by the sensor of a crash requiring deployment of the airbag(s), and a system for permitting the occupant to be displaced away from the side door upon inflation of the airbag(s) and thereby increase the space between the occupant and the side door. | ||||||
| 205 | Portable laser digitizing system for large parts | US904225 | 1997-07-31 | US6069700A | 2000-05-30 | Fredrick C. Rudnick; Jeffrey M. Hansen; Charles M. Richards |
| A system for producing high accuracy surface scans of large and/or complex parts using a host machine such a machine for milling the part, a digitizing head attached to the host machine, and a remote laser tracking system for tracking the position of a retroreflector cube attached to the digitizing head. | ||||||
| 206 | Projectile tracking system | US136029 | 1998-08-18 | US6057915A | 2000-05-02 | Mark Squire; Murray Dunn; George Houghton |
| A projectile tracking system for acquiring and precisely tracking a projectile in flight in order to reveal the source from which the projectile was fired. The source is revealed by the back projection of a 3-dimensional track file. The system is particularly suited for tracking a bullet fired by a sniper and identifying the location of the sniper. Projectiles of interest typically become hot due to aerodynamic heating. A telescope focuses infrared light from a relatively large field of view on to an infrared focal plane array. In a detection mode, the system searches for the infrared signature of the projectile. The telescope's field of view is steered in the azimuth by a step and stare mirror which is driven by an azimuth drive motor mounted on the frame. When a projectile is detected, the system switches to a tracking mode and the mirror is steered by the azimuth drive motor and a pivot motor to track the projectile. A laser radar system provides a laser beam which is optically coaligned with the telescope axis. Mirror angular position information, laser radar pulse travel time, and the missile spot position on detector array are used by a computer to calculate projectile trajectory information and to determine the origin of the projectile using known ballistic trajectory methods. Although only a small portion of the total trajectory may be captured, the very accurate position information permits extrapolation to determine the launch point of the projectile. | ||||||
| 207 | Laser distance finding apparatus | US959598 | 1997-10-29 | US5991011A | 1999-11-23 | Hartmut Damm |
| A laser range finding apparatus 10 comprises a pulsed laser 12, a light deflecting device 14, photo-receiver arrangement 16 and a reference object 18 arranged at a defined spacing from the light deflecting device 14. In this respect the reference object 18 has at least one triple element consisting of three mirror surfaces arranged at an angle of 90.degree. to one another. | ||||||
| 208 | Optical identification and monitoring system using pattern recognition for use with vehicles | US474786 | 1995-06-07 | US5845000A | 1998-12-01 | David S. Breed; Wilbur E. DuVall; Wendell C. Johnson |
| A vehicle interior monitoring system to identify, locate and monitor occupants, including their parts, and other objects in the passenger compartment and objects outside of a motor vehicle, such as an automobile or truck, by illuminating the contents of the vehicle and objects outside of the vehicle with electromagnetic, and specifically infrared, radiation and using one or more lenses to focus images of the contents onto one or more arrays of charge coupled devices (CCD arrays). Outputs from the CCD arrays, are analyzed by appropriate computational means employing trained pattern recognition technologies, to classify, identify or locate the contents or external objects. In general, the information obtained by the identification and monitoring system is used to affect the operation of some other system in the vehicle. When system is installed in the passenger compartment of an automotive vehicle equipped with an airbag, the system determines the position of the vehicle occupant relative to the airbag and disables deployment of the airbag if the occupant is positioned so that he/she is likely to be injured by the deployment of the airbag. | ||||||
| 209 | Projectile tracking system | US667401 | 1996-06-21 | US5796474A | 1998-08-18 | Mark Squire; Howard Hyman; Richard Trissel; George Houghton; Daniel Leslie; Murray Dunn |
| The present invention provides a projectile tracking system for acquiring and precisely tracking a projectile in flight in order to reveal the source from which the projectile was fired. The source is revealed by the back projection of a 3-dimensional track file. The system is particularly suited for tracking a bullet fired by a sniper and identifying the location of the sniper. Projectiles of interest are typically traveling at a substantial fraction of the speed of sound or even faster than the speed of sound and therefore become hot due to aerodynamic heating. A telescope focuses infrared light from a relatively large field of view on to an infrared focal plane array. In a projectile detection mode, the system searches for the infrared signature of the fast moving projectile. The telescope's field of view is steered in the azimuth by a step and stare mirror which is driven by an azimuth drive motor mounted on the frame. When a projectile is detected the system switches to a tracking mode and the mirror is steered by the azimuth drive motor and a pivot motor to track the projectile. A short pulse high repetition rate laser in a laser radar system provides a pulsed laser beam which is optically coaligned with the telescope axis. Mirror angular position information, laser radar pulse travel time and the missile spot position on detector array are used by a computer to calculate bullet trajectory information and to determine the source or origin of the projectile using known ballistic trajectory methods. Although only a small portion of the total trajectory may be captured, the very accurate position information permits extrapolation to determine the launch point of the projectile. | ||||||
| 210 | Method and apparatus for a selective optical retroreflector | US534432 | 1995-09-27 | US5539565A | 1996-07-23 | Ray O. Waddoups; John S. Scavarda |
| An optical retroreflector apparatus and method detects (20) incident light radiation (12). A processor (30) periodically enables the detector (20, 60-64) to receive a signal included in the incident light radiation (12). A reflector (40) is triggered by receipt of a particular signal included in the incident light radiation to reflect a coded signal toward the source of the incident light radiation. | ||||||
| 211 | Optical motion sensor | US186310 | 1994-01-25 | US5463463A | 1995-10-31 | Dennis N. Harvey; Randal L. Jenniges |
| An apparatus determines the position of an object with respect to a reference coordinate system. Preferably, the apparatus includes a target attached to the object, the target moves within a defined region and has a surface with a first pattern thereon. A projection device projects a second pattern upon the surface. A sensing device provides an image signal indicative of the target surface including the first pattern and the second pattern. An analyzer receives the image signal and determines the position of the object based on the position of images of the first pattern and the second pattern. | ||||||
| 212 | Gated image intensifiers for active imaging of reflectors by day or night | US128496 | 1993-09-07 | US5408099A | 1995-04-18 | Dallas N. Barr; John E. Nettleton; Brian C. Redman; Clifton S. Fox |
| Lightweight low power IR locater for reflection enhanced targets with .apeq.20 microsecond pulsed IR diode laser and 26 40 microsecond synchronized range-gated image. | ||||||
| 213 | Three dimensional camera and range finder | US593243 | 1990-10-05 | US5081530A | 1992-01-14 | Antonio Medina |
| A three dimensional camera system in which a precisely timed beam of energy is emitted from a single source with the beam illuminating the scene. The reflected energy from the beam is detected with a camera whose sensitivity is precisely timed and synchronized with the emitted beam. The reflected energy is separated and segregated according to the time of arrival at the camera. One or more cycles of energy are emitted, the camera segregates reflected energy during each cycle by separately storing the energy detected before and after a given time. The ratio of two consecutive separately detected energies conveys depth or third dimension. Signals can be displayed to a viewer to create a stereoscopic image or used by a machine for automatic response to a three dimensional environment. | ||||||
| 214 | System for modelling low resolution atmospheric propagation | US383372 | 1989-07-17 | US5075856A | 1991-12-24 | Francis X. Kneizys; Eric P. Shettle; Leonard W. Abreu; James H. Chetwynd; Gail P. Anderson; William O. Gallery; John E. A. Selby; Shepard A. Clough |
| LOWTRAN 7 is a low-resolution propagation model and computer code for predicting atmospheric transmittance and background radiance from 0 to 50,000 cm.sup.- at a resolution of 20 cm.sup.-. The code is based on the LOWTRAN 6 (1983) model with a number of improvements. Multiple scattered radiation has been added to the model as well as new molecular band model parameters and new ozone and molecular oxygen absorption parameters for the UV. Other modifications include a wind-dependent desert model, new cirrus cloud models, and new cloud and rain models. The code also includes new representative (geographical and seasonal) atmospheric models and updated aerosol models with options to replace them with user-derived values. An improved extra-terrestrial solar source function is also included. Six modes of program execution are allowed with the new model and computer code for a given slant path geometry. | ||||||
| 215 | サブ解像度での光学的検出 | JP2015004519 | 2015-01-13 | JP6359466B2 | 2018-07-18 | ロマノ ニタイ; グロスィンガー ナダヴ; アロン エミル; アルペルン ヤイル |
| 216 | LIDARシステム及びIRカメラシステム用の範囲拡大 | JP2015193447 | 2015-09-30 | JP2016099340A | 2016-05-30 | ダグラス・アール・ユングヴィルト |
| 【課題】光検出と測距(LIDAR)デバイスを含むシステム。 【解決手段】システムは、LIDARターゲットを更に含む。LIDARデバイスは、LIDARターゲットに光ビームを向ける。システムは、LIDARターゲットに接触する逆反射物質も含む。 【選択図】図1 |
||||||
| 217 | レーザレーダ装置、惑星着陸用セーフランディングセンサ、宇宙機用ドッキングセンサ、宇宙ごみ回収センサおよび車載衝突防止センサ | JP2013543983 | 2011-11-15 | JPWO2013072956A1 | 2015-04-02 | 俊平 亀山; 勝治 今城; 論季 小竹; 秀伸 辻; 秀晃 落水; 幹夫 高林; 平野 嘉仁; 嘉仁 平野 |
| ターゲットへの送信光を出力するパルスレーザ2と、送信光を所定のビーム拡がり角とする送信光学系3と、ターゲットからの散乱光を受光し、電気信号に変換する受光素子アレイ7と、電気信号から受信強度および受信時間を検出する電気回路アレイ8と、受信時間に基づいて、ターゲットまでの距離またはターゲットの3次元形状を計測する距離・3次元形状出力部91と、受信強度および受信時間に基づいて、ビーム拡がり角を変更するかを判定する判定部92と、判定結果に基づいて、ビーム拡がり角を変更する制御部10とを備えた。 | ||||||
| 218 | 測距装置及びプログラム | JP2013097863 | 2013-05-07 | JP2014219250A | 2014-11-20 | TEZUKA KOICHI; IIDA KOICHI; MORIKAWA TAKESHI |
| 【課題】回路規模を増大させることなく、近距離に位置する測定対象物の測距精度を高めること。【解決手段】測距装置は、光源と、前記光源からの光線を反射することにより外部に出射し、前記光線の出射方向が変化するように角度が制御される第1走査ミラーと、受光素子と、外部から入射する光線を前記受光素子に向けて反射し、外部の複数方向から入射する光線のうち、前記受光素子に受光される方向の光線が変化するように角度が制御される第2走査ミラーと、外部に存在する測定対象物までの距離を算出する距離測定部と、前記測定対象物までの距離に関する距離情報と、前記光線の出射時の前記第1走査ミラーの角度に関する角度情報とに基づいて、前記第2走査ミラーの角度を制御する制御装置とを含む。【選択図】図1 | ||||||
| 219 | 運搬機械の位置調整支援システム | JP2013507613 | 2012-03-27 | JPWO2012133410A1 | 2014-07-28 | 菅原 一宏; 一宏 菅原; 小倉 弘; 弘 小倉; 田中 克明; 克明 田中; 輝雄 中村 |
| 【課題】運搬機械が積込機械による積込作業に最適な位置及び方向となるように相対位置決めする際における有効な支援を行う。【解決手段】掘削機械1に対してダンプトラック2を目標となる積込作業が行われる位置に迅速かつ円滑に進行するために、ダンプトラック2を掘削機械1に対して積込目標位置に配置して、ダンプトラック2のGPS受信機32でGPS衛星30から地理的位置を検出して、その位置と方向とを目標位置画像P1として掘削機械1に送信して、以後のダンプトラック2の進入時に、このダンプトラック2のディスプレイ36に目標位置画像P1とそれへの進入ルートRとを表示し、進入ルートRに沿って現位置画像P2が目標位置画像P1に進行するようにダンプトラック2を運転することによって、ダンプトラック2を設定した積込目標位置に配置する。【選択図】図3 | ||||||
| 220 | Opto-electronic scanner | JP2013229207 | 2013-11-05 | JP2014098696A | 2014-05-29 | GREGOR HUBER; MARTIN KUFNER; BORIS SZERBAKOWSKI; SCHMITZ STEPHAN |
| PROBLEM TO BE SOLVED: To provide an opto-electronic scanner which has a higher signal/noise ratio and improved resistance to external light.SOLUTION: The opto-electronic scanner for monitoring a target area comprises a light transmitter for transmitting optical signals, a light deflecting unit for deflecting the optical signals transmitted by the light transmitter into the target area, a light receiver for receiving light reflected from an object being in the target area to be monitored, and a controller for generating optical signals and/or influencing optical signals. Each of the optical signals transmitted into the target area by the light transmitter is generated based on, in particular, an output signal modulated by a frequency band spreading method and/or a matched filter method. The output signal is represented as a binary signal comprising zeros and ones, and this output signal includes more zeros than ones. | ||||||
QQ群二维码
意见反馈
意见反馈