TWI518329B - Optical system for detecting wind - Google Patents

Optical system for detecting wind Download PDF

Info

Publication number
TWI518329B
TWI518329B TW103141806A TW103141806A TWI518329B TW I518329 B TWI518329 B TW I518329B TW 103141806 A TW103141806 A TW 103141806A TW 103141806 A TW103141806 A TW 103141806A TW I518329 B TWI518329 B TW I518329B
Authority
TW
Taiwan
Prior art keywords
measurement system
target
laser light
wind measurement
voltage
Prior art date
Application number
TW103141806A
Other languages
Chinese (zh)
Other versions
TW201621321A (en
Inventor
廖子毅
林榮貴
江智偉
Original Assignee
財團法人工業技術研究院
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 財團法人工業技術研究院 filed Critical 財團法人工業技術研究院
Priority to TW103141806A priority Critical patent/TWI518329B/en
Priority to CN201410776663.2A priority patent/CN105759072B/en
Application granted granted Critical
Publication of TWI518329B publication Critical patent/TWI518329B/en
Publication of TW201621321A publication Critical patent/TW201621321A/en

Links

Landscapes

  • Optical Radar Systems And Details Thereof (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)

Description

光學式測風系統 Optical wind measurement system

本發明為一種光學式測風系統,尤指一種以連續波雷射光搭配光學聚焦系統取代同調脈衝雷射、以電壓偵測取代傅立葉頻譜分析、以單鏡單視野與光電陣列之組合取代多軸掃描系統及單鏡單視野以形成一極小之觀測區而可避免寬視野在複雜地形區域之誤差之光學式測風系統。 The invention relates to an optical wind measurement system, in particular to replacing a coherent pulse laser with a continuous wave laser light and an optical focusing system, replacing the Fourier spectrum analysis with a voltage detection, and replacing the multi-axis with a single mirror single field and a photoelectric array. An optical wind measurement system that scans the system and single-mirror single field of view to form a very small viewing area that avoids errors in wide field of view in complex terrain areas.

傳統風機係以尾置風速風向計進行測風,以控制風機指向。近年來,有利用雷射進行測風,然習知雷射測風系統之問題主要包含系統複雜、單價極高及需有寬視野。 Conventional fans use the tail wind speed and direction meter to measure the wind to control the fan pointing. In recent years, there have been the use of lasers for wind measurement. However, the problems of the conventional laser measurement system mainly include complex systems, high unit prices, and a wide field of view.

針對系統複雜與單價極高部份,請參閱圖1所示,習知測風系統採用立體掃描,其偵測範圍呈現一錐形體,如圖1虛線區域所示,錐形體會隨著距離而急速擴張,於複雜地形環境容易受到地形阻擋,而在多塔架風機環境則容易受到其他風機阻擋,皆會影響偵測結果。此外,習知測風系統屬干涉放大架構,在都卜勒雷射測風技術出現之後,將雷射設置於機艙上,可量測風機前緣數百公尺處之風場,有效避免葉片流場之干擾。但是都卜勒系統需使用脈衝式同調(coherence)雷射,同時系統需即時進行傅立葉運算,其頻譜技術需使用高速傅立葉轉換,而資料偵測/分析需使用高速運算主機,高運算需求、高功率消耗、高耗材成本,整體設備非常複雜,且單價極高,約需25000~35000歐元,且壽命短,一般不高於三年。因此無法普遍於風機配置。 For the complexity of the system and the extremely high unit price, please refer to Figure 1. The conventional wind measurement system adopts stereo scanning, and its detection range presents a cone. As shown by the dotted line in Figure 1, the cone will follow the distance. Rapid expansion, it is easy to be blocked by terrain in complex terrain, and it is easy to be blocked by other fans in multi-tower fan environment, which will affect the detection results. In addition, the conventional wind measurement system is an interference amplification structure. After the emergence of the Doppler laser wind measurement technology, the laser is placed on the nacelle, and the wind field at the front edge of the fan can be measured hundreds of meters, effectively avoiding the blade. Interference from the flow field. However, the Doppler system needs to use a pulse coherence laser. At the same time, the system needs to perform Fourier operation in real time. The spectrum technology needs to use high-speed Fourier transform, and the data detection/analysis needs to use high-speed computing host, high computing demand and high. Power consumption, high consumables cost, the overall equipment is very complicated, and the unit price is extremely high, about 25,000~35,000 euros, and the life is short, generally not more than three years. Therefore, it is not universally applicable to the fan configuration.

其次,針對需有寬視野部份,由於都卜勒系統是在雷射路徑上量測風速分量,對於風向之偵測需以不同夾角之雷射指向以獲得風的方向,因此這個夾角越大越好。但是如此在數百公尺外會 形成一個很寬的觀測區,在有地形效應的地方,會有方位誤判的潛在問題。 Secondly, for the need to have a wide field of view, since the Doppler system measures the wind speed component on the laser path, the detection of the wind direction needs to be directed at different angles to obtain the direction of the wind, so the larger the angle it is good. But this will be hundreds of meters away. Forming a wide observation area, where there is a topographic effect, there is a potential problem of misjudgment.

此外,習知測風系統是以風速量測為優先。例如已知一種風速偵測系統,該系統未設置聚焦裝置,且其使用分軸發射/接收,因此需要特定的交會位置,此外,該系統未使用單一光路,照明區域與強度無法校正,因此必須使用峰值偵測(peak detection),但如此可能會偵測到獨立事件,影響偵測的準確度。 In addition, the conventional wind measurement system takes priority in measuring the wind speed. For example, a wind speed detecting system is known which does not have a focusing device, and uses split transmission/reception, so a specific intersection position is required. In addition, the system does not use a single optical path, and the illumination area and intensity cannot be corrected, so Use peak detection, but this may detect independent events and affect the accuracy of the detection.

據此,相關技術領域人士亟需一種「簡化雷射源、簡化運算、簡化觀測區且具有窄視野」之光學式測風系統,以解決習知相關問題,並可增加測風市場競爭力效果。 Accordingly, there is a need in the related art to provide an optical wind measurement system that "simplifies the laser source, simplifies the calculation, simplifies the observation area, and has a narrow field of view" to solve the related problems and increase the competitiveness of the wind measurement market. .

在一實施例中,本發明提出一種光學式測風系統,包含一光源、一透鏡單元、一感測單元及一處理單元;光源用以發射連續波雷射光;透鏡單元為單鏡單視野,透鏡單元具有相對之一第一側與一第二側,連續波雷射光由第一側射入透鏡單元,於第二側形成一擴束之連續波雷射光,擴束之連續波雷射光聚焦於一偵測位置並回傳一回波訊號;感測單元設置於透鏡單元之第一側,上述回波訊號通過透鏡單元投影至感測單元並產生電壓訊號;處理單元耦接於感測單元,由處理單元根據電壓訊號之電壓變化而計算一目標物之走向。 In one embodiment, the present invention provides an optical wind measurement system including a light source, a lens unit, a sensing unit, and a processing unit; the light source is configured to emit continuous wave laser light; and the lens unit is a single mirror single field of view. The lens unit has a first side and a second side opposite to each other, and the continuous wave laser light is incident on the lens unit from the first side, and forms a beam-expanded continuous-wave laser light on the second side, and the expanded-wave continuous laser light is focused. The sensing unit is disposed on the first side of the lens unit, and the echo signal is projected to the sensing unit through the lens unit to generate a voltage signal; the processing unit is coupled to the sensing unit The processing unit calculates the direction of a target according to the voltage change of the voltage signal.

100‧‧‧光學式測風系統 100‧‧‧Optical wind measurement system

10‧‧‧光源 10‧‧‧Light source

200‧‧‧目標物 200‧‧‧ Targets

20‧‧‧透鏡單元 20‧‧‧ lens unit

21‧‧‧第一側 21‧‧‧ first side

22‧‧‧第二側 22‧‧‧ second side

23‧‧‧觀測區 23‧‧‧ observation area

30‧‧‧感測單元 30‧‧‧Sensor unit

31‧‧‧成像面 31‧‧‧ imaging surface

40‧‧‧處理單元 40‧‧‧Processing unit

4A、4B、4C‧‧‧影像變化 4A, 4B, 4C‧‧‧ image changes

L10‧‧‧連續波雷射光 L10‧‧‧Continuous wave laser light

L20‧‧‧擴束之連續波雷射光 L20‧‧‧Expanded continuous wave laser light

P‧‧‧偵測位置 P‧‧‧Detection location

S‧‧‧回波訊號 S‧‧‧ echo signal

W‧‧‧寬度 W‧‧‧Width

圖1為習知風機之測風 Figure 1 shows the wind measurement of a conventional fan

圖2為本發明之一實施例之架構示意圖。 2 is a schematic block diagram of an embodiment of the present invention.

圖3為本發明進行測風之流程示意圖。 FIG. 3 is a schematic flow chart of measuring wind in the present invention.

圖4為本發明之回波訊號於感測單元成像之示意圖。 4 is a schematic diagram of an echo signal of the present invention imaged by a sensing unit.

請參閱圖2及圖3所示實施例,本發明之一種光學式測風系統100,包含一光源10、一透鏡單元20、一感測單元30及一處理單元40。 Referring to the embodiment shown in FIG. 2 and FIG. 3 , an optical wind measurement system 100 of the present invention includes a light source 10 , a lens unit 20 , a sensing unit 30 , and a processing unit 40 .

光源10可發射一連續波雷射光,例如,可採用雷射半導體作 為光源10,用以發射出非同調連續波之連續波雷射光L10。 The light source 10 can emit a continuous wave of laser light, for example, a laser can be used. It is a light source 10 for emitting continuous wave laser light L10 of a non-coherent continuous wave.

透鏡單元20為單鏡單視野,透鏡單元20具有相對之一第一側21與一第二側22,連續波雷射光L10由第一側21射入透鏡單元,於第二側22形成一擴束之連續波雷射光L20,該擴束之連續波雷射光L20可聚焦於一偵測位置P並回傳一回波訊號S。偵測位置P可依所需而設定,例如,變換具有不同焦距的透鏡,即可不同的偵測位置P,例如300公尺或其他距離,或可使用變焦透鏡,以變換不同之聚焦位置。其次,擴束之連續波雷射光L20可於第二側22形成一極小的觀測區23,觀測區23之寬度W約位於5~30公分之範圍,相較於習知呈錐形外擴之觀測區,本發明以單光束、單視野形成一極小之觀測區,可避免被其他風機或地形之干擾。而當回傳回波訊號S時,回波訊號S先通過透鏡單元20,再投影至感測單元30。 The lens unit 20 is a single mirror single field of view. The lens unit 20 has a first side 21 and a second side 22 opposite to each other. The continuous wave laser light L10 is incident on the lens unit from the first side 21 and forms an expansion on the second side 22. The bundle of continuous wave laser light L20, the expanded continuous wave laser light L20 can be focused on a detection position P and return an echo signal S. The detection position P can be set as desired, for example, by changing lenses having different focal lengths, that is, different detection positions P, for example, 300 meters or other distances, or a zoom lens can be used to change different focus positions. Secondly, the expanded continuous-wave laser light L20 can form a very small observation area 23 on the second side 22, and the width W of the observation area 23 is approximately in the range of 5 to 30 cm, which is similar to the conventional conical expansion. In the observation area, the invention forms a very small observation area with a single beam and a single field of view, so as to avoid interference by other fans or terrain. When the echo signal S is returned, the echo signal S passes through the lens unit 20 and is then projected to the sensing unit 30.

感測單元30具有一成像面31,回波訊號S投影於成像面31並產生一電壓訊號,而電壓訊號之強弱會依位於偵測位置P之空間物件之變化而不同。就大氣環境而言,其含有各種物質,例如氣團、水霧,細至氣團中的粒子,以下統稱為目標物200。請參閱圖2所示,目標物200隨空氣飄動,當目標物200飄至擴束之連續波雷射光L20之照射範圍且擴束之連續波雷射光L20照射到目標物200時,回波訊號會增強,亦即電壓較強,而當目標物200繼續飄動並脫離擴束之連續波雷射光L20之照射範圍後,擴束之連續波雷射光L20照射到大氣環境中不具有目標物200之區域時,回波訊號則會減弱,亦即電壓較低,因此可於感測單元30形成明暗不同的影像。 The sensing unit 30 has an imaging surface 31. The echo signal S is projected on the imaging surface 31 to generate a voltage signal, and the strength of the voltage signal varies according to the change of the spatial object located at the detection position P. In the case of the atmospheric environment, it contains various substances such as air masses, water mist, and fine particles in the air mass, hereinafter collectively referred to as target 200. Referring to FIG. 2, the target object 200 flutters with the air, and when the target object 200 floats to the illumination range of the expanded continuous wave laser light L20 and the expanded continuous wave laser light L20 illuminates the target object 200, the echo signal It will be enhanced, that is, the voltage is strong, and after the target object 200 continues to flutter and escapes the illumination range of the expanded beam of the continuous wave laser light L20, the expanded beam of the continuous wave laser light L20 is irradiated to the atmosphere without the target object 200. In the region, the echo signal is weakened, that is, the voltage is low, so that the sensing unit 30 can form an image with different brightness and darkness.

請參閱3及圖4所示,處理單元40耦接於感測單元30,可由處理單元40根據於一段時間內之電壓訊號之電壓變化而計算目標物200之走向。圖4顯示於時間大約為5秒、9秒及20秒左右時,分別有一目標物進入偵測位置,因此導致電壓訊號出現影像變化4A、4B、4C,影像變化4A、4B、4C之矩形格分別代表擴束之連續波雷射光L20照射到目標物200時所形成之影像。就影像變化 4A而言,該矩形格代表目標物200於大約19秒時進入偵測位置P,於大約21秒時離開偵測位置P,然其距離始終維持於大約1.5公里,並未產生偏移,代表風機之朝向與風向一致,影像變化4B同理。而就影像變化4C而言,該矩形格代表目標物200於大約7秒時進入偵測位置P,於大約11秒時離開偵測位置P,而其距離由大約2.3公里偏移至2.2公里,代表風機之朝向與風向不一致。油處理單元40計算電壓訊號之二電壓變化之時間差,及可推求目標物200之走向。處理單元40可採用可程式控制(PLC控制),以擴束之連續波雷射光L20對目標物200之回波訊號S剖面進行追蹤,並以電壓差分及電壓偵測進行運算,從而獲得目標物200之移動方向與速度。感測單元30之形式不限,例如可採用光電陣列,且可於成像面31以光電陣列區別左右像位置,以形成左右兩個觀測區,藉此辨識目標物200之左右側。此外,可設定處理單元40擷取電壓訊號之時間段。 Referring to FIG. 3 and FIG. 4, the processing unit 40 is coupled to the sensing unit 30, and the processing unit 40 can calculate the direction of the target 200 according to the voltage change of the voltage signal over a period of time. Figure 4 shows that when the time is about 5 seconds, 9 seconds, and 20 seconds, there is a target entering the detection position, thus causing image changes of the voltage signal 4A, 4B, 4C, and the rectangular changes of the image changes 4A, 4B, 4C. The images formed by the continuous beam laser light L20 that is expanded to the target object 200 are respectively reflected. Image change For 4A, the rectangular grid represents that the target object 200 enters the detection position P at about 19 seconds, and leaves the detection position P at about 21 seconds, but the distance is always maintained at about 1.5 kilometers, and no offset occurs. The orientation of the fan is consistent with the wind direction, and the image change 4B is the same. In the case of image change 4C, the rectangular grid represents that the target 200 enters the detection position P at about 7 seconds, and leaves the detection position P at about 11 seconds, and the distance is shifted from about 2.3 kilometers to 2.2 kilometers. The direction of the fan is inconsistent with the direction of the wind. The oil processing unit 40 calculates the time difference between the voltage changes of the voltage signals and the direction of the target 200. The processing unit 40 can use programmable control (PLC control) to track the echo signal S profile of the target object 200 by expanding the continuous wave laser light L20, and perform calculation by voltage difference and voltage detection to obtain the target object. The direction and speed of movement of 200. The form of the sensing unit 30 is not limited. For example, a photoelectric array may be employed, and the left and right image positions may be distinguished by the photoelectric array on the imaging surface 31 to form two left and right observation regions, thereby identifying the left and right sides of the target 200. In addition, the time period during which the processing unit 40 captures the voltage signal can be set.

綜上所述,本發明所提供之光學式測風系統,以連續波雷射光搭配光學聚焦系統取代同調脈衝雷射、以電壓偵測取代傅立葉頻譜分析、以單鏡單視野與光電陣列之組合取代多軸掃描系統及單鏡單視野以形成一極小之觀測區,無須使用立體掃描,空間投影(footprint)近乎一致,因而可避免寬視野在複雜地形區域之誤差,可在多塔架風機與複雜地形環境使用,無須頻譜技術,沒有高速運算需求,資料偵測可以簡化為電位偵測,DSP/嵌入式系統即可勝任運算量。經驗證,以本發明之架構可達成單一測點(500~1500公尺@5mW),資料傳輸率(data rate)少於五秒,角解析度(水平)約為1度,風速誤差小於0.5公尺/秒(m/s),造價低於新台幣45萬元(約合11000歐元)。據此可知,本發明確具有可達成「簡化雷射源、簡化運算、簡化觀測區且具有窄視野」之作用,可解決習知測風系統複雜、單價極高及需有寬視野問題,可降低測風系統單價成本、系統複雜度以及方位誤判,進而提高市場競爭力。 In summary, the optical wind measurement system provided by the present invention replaces the coherent pulse laser with continuous wave laser light and optical focusing system, replaces Fourier spectrum analysis with voltage detection, and combines single mirror single field and photoelectric array. Replacing the multi-axis scanning system and single-mirror single-field to form a very small observation area, without the need for stereo scanning, the spatial footprint is nearly uniform, thus avoiding the error of wide field of view in complex terrain areas, and can be used in multi-tower fans The use of complex terrain environment, no need for spectrum technology, no high-speed computing requirements, data detection can be simplified to potential detection, DSP / embedded system can be competent for computing. It has been verified that a single measuring point (500~1500 meters @5mW) can be achieved with the architecture of the invention, the data rate is less than five seconds, the angular resolution (horizontal) is about 1 degree, and the wind speed error is less than 0.5. Metrics per second (m/s), the cost is less than NT$450,000 (approximately 11,000 Euros). Accordingly, the present invention has the effect of "simplifying the laser source, simplifying the calculation, simplifying the observation area, and having a narrow field of view", and can solve the problem that the conventional wind measurement system is complicated, the unit price is extremely high, and a wide field of view is required. Reduce the unit cost, system complexity and azimuth misjudgment of the wind measurement system, thereby improving market competitiveness.

惟以上所述之具體實施例,僅係用於例釋本發明之特點及功 效,而非用於限定本發明之可實施範疇,於未脫離本發明上揭之精神與技術範疇下,任何運用本發明所揭示內容而完成之等效改變及修飾,均仍應為本發明之申請專利範圍所涵蓋。 However, the specific embodiments described above are merely used to illustrate the features and functions of the present invention. The invention is not intended to limit the scope of the invention, and any equivalent changes and modifications made by the disclosure of the present invention should still be the present invention without departing from the spirit and scope of the invention. The scope of the patent application is covered.

100‧‧‧光學式測風系統 100‧‧‧Optical wind measurement system

10‧‧‧光源 10‧‧‧Light source

200‧‧‧目標物 200‧‧‧ Targets

20‧‧‧透鏡單元 20‧‧‧ lens unit

30‧‧‧感測單元 30‧‧‧Sensor unit

40‧‧‧處理單元 40‧‧‧Processing unit

Claims (8)

一種光學式測風系統,其包含有:一光源,用以發射連續波雷射光;一透鏡單元,該透鏡單元具有相對之一第一側與一第二側,該連續波雷射光由該第一側射入該透鏡單元,於該第二側形成一擴束之連續波雷射光,擴束之連續波雷射光聚焦於一偵測位置並回傳一回波訊號;一感測單元,設置於該透鏡單元之該第一側,上述該回波訊號通過該透鏡單元投影至該感測單元並產生一電壓訊號;以及一處理單元,耦接於該感測單元,由該處理單元根據該電壓訊號之電壓變化而計算一目標物之走向,該目標物為大氣環境所含之物質且可隨空氣飄動,藉由該目標物之走向以推算出風向及風速。 An optical wind measurement system comprising: a light source for emitting continuous wave laser light; a lens unit having a first side and a second side opposite to each other, the continuous wave of the laser light One side of the lens unit is incident on the second side to form a beam-expanded continuous-wave laser light, and the expanded continuous-wave laser light is focused on a detection position and returns an echo signal; a sensing unit is disposed And the processing unit is coupled to the sensing unit, and the processing unit is configured according to the sensing unit The voltage of the voltage signal changes to calculate the direction of a target. The target is a substance contained in the atmospheric environment and can float with the air, and the direction of the target is used to calculate the wind direction and the wind speed. 如申請專利範圍第1項所述之光學式測風系統,其中該感測單元為光電陣列,該光電陣列具有一成像面,該回波訊號投影於該成像面。 The optical wind measurement system of claim 1, wherein the sensing unit is a photoelectric array, and the photoelectric array has an imaging surface, and the echo signal is projected on the imaging surface. 如申請專利範圍第2項所述之光學式測風系統,其中以該光電陣列區別左右像位置,以形成左右兩個觀測區。 The optical wind measurement system according to claim 2, wherein the left and right image positions are distinguished by the photoelectric array to form two left and right observation regions. 如申請專利範圍第1項所述之光學式測風系統,其中該透鏡單元於該第二側形成一觀測區,該觀測區之寬度位於5~30公分之範圍。 The optical wind measurement system of claim 1, wherein the lens unit forms an observation area on the second side, and the width of the observation area is in the range of 5 to 30 cm. 如申請專利範圍第1項所述之光學式測風系統,其中該處理單元係計算該電壓訊號之二電壓變化之時間差,以推求該目標物之走向。 The optical wind measurement system of claim 1, wherein the processing unit calculates a time difference of the voltage change of the voltage signal to estimate the direction of the target. 如申請專利範圍第1項所述之光學式測風系統,其中該處理單元採用可程式控制(PLC控制),以該連續波雷射光對該目標物之回波訊號剖面進行追蹤,並以電壓差分及電壓偵測進行運算,從而獲得該目標物之移動方向與速度。 The optical wind measurement system according to claim 1, wherein the processing unit uses programmable control (PLC control) to track the echo signal profile of the target with the continuous wave laser light, and the voltage is The differential and voltage detection operations are performed to obtain the moving direction and speed of the target. 如申請專利範圍第1項所述之光學式測風系統,其中該光源為雷射半導體,用以發射出非同調之連續波雷射光。 The optical wind measurement system of claim 1, wherein the light source is a laser semiconductor for emitting non-coherent continuous wave laser light. 如申請專利範圍第1項所述之光學式測風系統,其中該目標物為氣團、水霧或氣團中的粒子。 The optical wind measurement system of claim 1, wherein the target is a particle in a gas mass, a water mist or an air mass.
TW103141806A 2014-12-02 2014-12-02 Optical system for detecting wind TWI518329B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
TW103141806A TWI518329B (en) 2014-12-02 2014-12-02 Optical system for detecting wind
CN201410776663.2A CN105759072B (en) 2014-12-02 2014-12-15 Optical anemometry system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW103141806A TWI518329B (en) 2014-12-02 2014-12-02 Optical system for detecting wind

Publications (2)

Publication Number Publication Date
TWI518329B true TWI518329B (en) 2016-01-21
TW201621321A TW201621321A (en) 2016-06-16

Family

ID=55640415

Family Applications (1)

Application Number Title Priority Date Filing Date
TW103141806A TWI518329B (en) 2014-12-02 2014-12-02 Optical system for detecting wind

Country Status (2)

Country Link
CN (1) CN105759072B (en)
TW (1) TWI518329B (en)

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0194221A (en) * 1987-10-06 1989-04-12 Hamamatsu Photonics Kk Object state detector
JPH04184123A (en) * 1990-11-16 1992-07-01 Hitachi Ltd Physical quantity sensor
CN100348980C (en) * 2005-01-18 2007-11-14 浙江大学 Two-phase flow digital particle image speed measurement method and device
GB0616837D0 (en) * 2006-08-25 2006-10-04 Moir Christopher I Velocity detector
EP2175281A1 (en) * 2008-10-08 2010-04-14 Siemens Aktiengesellschaft Method and arrangement to determine a wind-speed
CN102667495A (en) * 2009-09-28 2012-09-12 喷特路姆科技有限公司 Methods, devices and systems for remote wind sensing
FR2951275B1 (en) * 2009-10-09 2012-11-02 Epsiline DEVICE FOR MEASURING WIND SPEED
CN102192707B (en) * 2010-03-04 2013-11-27 阿自倍尔株式会社 Physical quantity transducer and physical quantity measuring method
US9851444B2 (en) * 2012-09-14 2017-12-26 Mitsubishi Electric Corporation Laser radar device and method of calculating speed of object to be measured
CN103063869B (en) * 2012-12-27 2014-09-24 中国科学院安徽光学精密机械研究所 Measuring device and measuring method of light propagation path transverse average wind speed and wind direction
CN203655539U (en) * 2013-12-27 2014-06-18 华北电力大学(保定) Automatic wind detecting device of novel wind driven generator
CN104049105A (en) * 2014-07-02 2014-09-17 中冶赛迪工程技术股份有限公司 Method for measuring indoor natural wind velocity through optical fiber Doppler

Also Published As

Publication number Publication date
CN105759072B (en) 2020-04-14
TW201621321A (en) 2016-06-16
CN105759072A (en) 2016-07-13

Similar Documents

Publication Publication Date Title
CN109164430B (en) System and method for detecting position and posture of target by using laser echo and light spot
US10254404B2 (en) 3D measuring machine
JP5016245B2 (en) Measurement system for determining the six degrees of freedom of an object
CN211653129U (en) Two-dimensional scanning device and laser radar device with same
RU2523092C2 (en) Method and apparatus for measuring profile of spherical incurved, particularly, cylindrical bodies
JP2016516196A (en) Structured optical scanner correction tracked in 6 degrees of freedom
WO2005100911A2 (en) An apparatus and method for optical determination of intermediate distances
CN205091463U (en) Laser radar scans detecting device
CN106597461A (en) Two-dimensional scanning range-finding device
CN105572683A (en) Laser radar acquisition and ranging apparatus and working method thereof
CN105068082A (en) Laser radar scanning detection method and device
JP2002139304A (en) Distance measuring device and distance measuring method
CN106226782A (en) A kind of apparatus and method of air wind speed profile detection
CN102980534B (en) The non-contact measurement method of a kind of hidden rotating shaft and end face squareness and system
CN110470608A (en) A kind of method and device using polarization imaging measurement object smoothness
CN109579744A (en) Trailing type three-dimensional photoelectric auto-collimation method and apparatus based on grating
CN104931725A (en) Multi-point interference type rayleigh scattering-based speed measurement apparatus for flow field capable of simultaneously measuring two orthogonal components
TWI518329B (en) Optical system for detecting wind
CN104316022A (en) Improved compact precision laser triangulation rangefinder
CN108398104B (en) photoelectric dynamic angle measuring device capable of reducing random error and method thereof
CN115824170A (en) Method for measuring ocean waves by combining photogrammetry and laser radar
Savelyev et al. Stereo thermal marking velocimetry
CN103697825A (en) System and method of utilizing super-resolution 3D (three-dimensional) laser to measure
US10760894B2 (en) Optical detecting device capable of determining relative position of a reference object or a light source
Uriarte et al. Modeling distance nonlinearity in tof cameras and correction based on integration time offsets