今天在這里分享紅外與激光工程英文摘要寫作規范，這是一本3大核心收錄的刊物，是綜合性科技期刊，主要征收國內光學、光電子及交叉學科的學術論文與工程研究報告，集中反映了我國光學工程及光電技術在航空、航天等國防工業，以及國民經濟各個領域的工程應用水平。

　　紅外與激光工程征稿方向/欄目信息如下：

　　紅外技術及應用，激光器與激光光學，光電測量，光學設計，光學制造，光學器件，材料與薄膜，全息，光學成像技術，光通信與光傳感，光譜學，物理光學，非線性光學，超快光學，微納光學，生物光學，量子光學，集成光學，表面光學，大氣光學，海洋光學，空間光學等。

　　《紅外與激光工程》“英文長摘要”格式要求——綜述

　　一、篇幅：

　　英文長摘要篇幅要求在 600~800 字(單詞數)，須用第三人稱撰寫。

　　二、結構：

　　(1)題目、作者和單位(中英文信息須對應)

　　(2)英文長摘要正文(英文摘要中切忌使用“In this paper……”等)

　　1)研究意義(Significance)(突出本領域研究的重要性)

　　2)研究進展(Progress)(本領域的重要研究進展)：請標示出所對應的正

　　文中的圖表，以括號標注，如 (Fig.3)、(Tab.2) 等

　　3)結論與展望(Conclusions and Prospects)

　　(3)關鍵詞(Key words)

　　三、不引用參考文獻、數學公式和化學式，如果有引用其他文章，建議轉述。

　　四、不得簡單重復引言和結論。如有縮寫，需給出全稱。

　　五、“英文長摘要”請放在文末。

　　《紅外與激光工程》“英文長摘要”格式要求——研究論文

　　一、篇幅：

　　英文長摘要篇幅要求在 600~800 字(單詞數)，須用第三人稱撰寫。

　　二、結構：

　　(1)題目、作者和單位(中英文信息須對應)

　　(2)英文長摘要正文(英文摘要中切忌使用“In this paper……”等)

　　1)研究目的(Objective)(突出所做工作的重要性和必要性)

　　2)研究方法(Methods)

　　3)創新性結果(Results and Discussions): 請標示出所對應的正文中的圖

　　表，以括號標注，如 (Fig.3)、(Tab.2) 等

　　4)結論(Conclusions)

　　(3)關鍵詞(Key words)

　　三、不引用參考文獻、數學公式和化學式，如果有引用其他文章，建議轉述。

　　四、不得簡單重復引言和結論。如有縮寫，需給出全稱。

　　五、“英文長摘要”請放在文末。

　　《紅外與激光工程》“英文長摘要”格式要求——快報

　　一、篇幅：

　　英文長摘要篇幅要求在 300~400 字(單詞數)，須用第三人稱撰寫。

　　二、結構：

　　(1)題目、作者和單位(中英文信息須對應)

　　(2)英文長摘要正文(英文摘要中切忌使用“In this paper……”等)

　　1)研究目的(Objective)(突出所做工作的重要性和必要性)

　　2)研究方法(Methods)

　　3)創新性結果(Results and Discussions): 請標示出所對應的正文中的圖

　　表，以括號標注，如 (Fig.3)、(Tab.2) 等

　　4)結論(Conclusions)

　　(3)關鍵詞(Key words)

　　三、不引用參考文獻、數學公式和化學式，如果有引用其他文章，建議轉述。

　　四、不得簡單重復引言和結論。如有縮寫，需給出全稱。

　　五、“英文長摘要”請放在文末。 英文長摘要模板見后

　　科研論文英文長摘要模板

　　Design of portable infrared target simulator system

　　Gao Hongwei1

　　,Yang Zhongming

　　2*

　　,Liu Hongbo

　　3

　　, Zhuang Xingang

　　3

　　,Liu

　　Zhaojun

　　2

　　1 Key Laboratory of Laser and Infrared System, Shandong University, Qingdao 266237, China;

　　2 School of Information Science and Engineering, Shandong University, Qingdao

　　266237, China;

　　3 The 41st Institute of China Electronics Technology Group Corporation, Qingdao

　　266555, China

　　Abstract

　　Objective Infrared target simulator is an important part of infrared target

　　simulation experiment. When the outgoing pupil of the collimation system

　　coincides with the incident pupil of the detection equipment, it can provide a

　　stable infinitely far simulated target for infrared detection equipment, and the

　　simulation results have the advantages of being accurate, controllable and

　　repeatable experiments, which are used to evaluate the performance and accuracy

　　of infrared detection equipment. There are important applications in radar test, infrared guidance, infrared tracking, etc. With the development of photoelectric

　　detection equipment sensor integration and miniaturization, multi-band sensors

　　have become the standard configuration of most photoelectric detection

　　equipment. Due to changes in the debugging environment and the use of the

　　environment, it is necessary to adjust it frequently, but most of the target

　　simulators in the laboratory are only equipped with a single-band light source, large size is not convenient to carry. Therefore, it is necessary to establish

　　multi-band and small-sized portable target simulators to meet the needs of

　　different usage environments. For this purpose, an off-axis reflective infrared

　　target simulator system is designed in this paper. Methods A portable infrared target simulation system is built in this paper. A 110

　　mm aperture parallel light tube of reflective structure is chosen as the collimation

　　system (Fig.2). The optical-mechanical thermal integration analysis of the system

　　is performed to determine the deformation variation of the primary and secondary

　　mirrors and mechanical structure caused by temperature difference (Fig.8). The

　　self-collimating interferometric detection method is mounted using a Zygo

　　interferometer (Fig.11), and the mounting results are judged by the PV and RMS

　　value results of the face shape measurement of the standard plane mirror (Fig.13). Results and Discussions The portable infrared target simulation system is

　　mounted using self-collimating interferometry, with PV value of 0.356λ and RMS

　　value of 0.047λ (Fig.13), which is better than λ/20, and the results are excellent

　　and meet the usage requirements. The results of Zernike coefficient analysis show

　　that the system aberrations are mainly out-of-focus, tilt and higher order

　　aberrations of more than 5 levels (Tab.5), and the adjustable target disc is

　　designed to compensate and improve the imaging quality. A portable infrared

　　target simulation system is built in the laboratory to test the optical path and

　　verify the imaging function of the system. The infrared camera and head are

　　placed at a distance of 10 m from the system, and the imaging results are shown

　　(Fig.14). The targets of different shapes can be clearly identified, and the imaging

　　function of the system satisfies the demand of simulating targets at infinity. Conclusions A portable infrared target simulation system with working

　　wavelengths of 3-5 μm and 8-14 μm is designed. The system is characterized by

　　simple structure, adjustable wavelength, rich target, clear and stable imaging. The

　　wavefront quality of the system is analyzed using Zemax software, and the PV

　　value of the central field of view is 0.0132λ and the RMS value was 0.0038λ in

　　the 4-μm band, and the PV value of the central field of view is 0.0044λ and the

　　RMS value is 0.0013λ in the 12-μm band. An optical-mechanical thermal analysis

　　of the collimation system is performed, and at a temperature difference of 30°C, the deformation caused by the mechanical structure is much larger than the

　　deformation of the primary and secondary mirrors themselves, reaching the order

　　of 10 μm, and the imaging results have obvious out-of-focus errors, which can be

　　compensated for the out-of-focus errors introduced by the temperature change by

　　refocusing the target disc with adjustable three-dimensional position. The

　　imaging function of the system is tested. For different shapes of targets, the

　　system can become a clear and identifiable image, providing a stable simulated

　　target for infrared detection equipment. Key words: optical engineering; target simulator; optical design; collimator

　　Funding projects: Natural Science Foundation of China (No.********)

　　綜述英文長摘要模板

　　A survey on laser intersatellite link: Current status,

　　trends, and prospects

　　Li Rui1, 2, 5

　　, Lin Baojun

　　1, 2, 3, 4, 5

　　, Liu Yingchun

　　1, 2, 5

　　, Shen Yuan

　　2, 5

　　, Dong Ming-ji2, 5

　　, Zhao Shuai2, 5

　　, Kong Chenjie

　　2, 5

　　, Liu Enquan

　　2, 5

　　, Lin Xia

　　2, 5

　　(1. University of Chinese Academy of Sciences, Beijing 100049, China;

　　2. Innovation Academy for Microsatellites, Chinese Academy of Sciences, Shanghai

　　200135, China;

　　3. ShanghaiTech University, Shanghai 201203, China

　　4. Aerospace Information Research Institute, Chinese Academy of Sciences, Beijing

　　100094, China

　　5. Shanghai Engineering Center for Microsatellites, Shanghai 201210, China)

　　Abstract:

　　Significance The high directionality and short wavelength of laser transmission in

　　space make it a promising direction for the next generation of satellite laser

　　communication. The laser intersatellite communication can achieve high

　　quality-of-service satellite communication with high transmission speed, wide

　　bandwidth, and high security, which can even improve the precision of satellite

　　ranging in space. The establishment of a satellite backbone network with laser

　　intersatellite links can achieve global management and control of satellites, greatly

　　improve its independence from the ground system, and expand the communication

　　capacity. Due to its advantages in improving the survivability, autonomy, mobility and

　　flexibility of satellite networks, the domestic "Star Network", "Hongyan", "Hongyun", "Xingyun" and "Space-Earth Integration" constellations and foreign "Kuiper", "Telesat" and "Starlink" networks have integrated laser inter-satellite links as one of

　　its core transmission link methods, laser communication terminals also become one of

　　the standard spacecraft payloads. It is foreseeable that inter-satellite communication

　　will continue to develop and transform from the radio wave era to the laser era, which

　　makes the survey on laser intersatellite links meaningful. Progress First, the technical fundaments is introduced, including the link

　　establishment modes, link modulation modes, and wavelengths. The inter-satellite

　　laser link establishment mainly relies on the three steps of pointing, acquiring, and

　　tracking, comprehensively called PAT system. The link modulation modes include

　　non-coherent and coherent communications. Compared with the non-coherent system, the coherent system has the advantages of high spectral efficiency. For medium and

　　high-orbit satellites that need to carry more complex and sophisticated communication

　　tasks, the laser inter-satellite link is mostly modulated by the coherent communication

　　system. Conversely, low-orbit satellite laser communication and deep space

　　exploration projects mainly use non-coherent modulation mode. To reduce the impact

　　of the solar background and solar scattering, the current laser communication mainly

　　considers the selection in the range of 500 nm to 2000 nm. Since ground

　　industrial-grade laser components mostly use 1550 nm wavelength laser as a standard

　　preparation, the communication technology can be migrated to the satellite network at

　　a relatively low cost. With the development of technology, the communication

　　systems of various countries are developing in a more compatible direction, that is, compatible with both 1064 nm and 1550 nm wavelengths. Countries have successfully carried out a number of on-orbit technology verifications

　　in the field of inter-satellite laser communication, and have entered the stage of

　　large-scale application. The survey finds that the current on-orbit technology

　　verification uses customized laser terminals to meet the specific needs of various tasks. Companies such as Mynaric, Hyperion Tech, Thales Alenia Space, and NICT have

　　begun to launch laser terminal products with higher speed, smaller mass and volume, and lower power consumption. These terminal products can adapt to the universal

　　requirements of similar multi-tasking. According to the different mission requirements

　　of different orbit heights, the current development status and plans of laser

　　communication achievements since 2015 is summarized (Tab. 1). Through the

　　comprehensive survey, this paper reveals the flexibility and modularity trends of laser

　　communication terminals, and four development trends of satellite laser

　　communication: standardization, compatibility, networking, and commercialization. In addition to being used as a carrier for information interaction, laser ranging can

　　obtain more accurate inter-satellite ranging values, stronger anti-interference and

　　anti-eavesdropping capabilities compared to traditional RF ranging solutions. The end

　　of this paper surveys on prospects of satellite laser ranging applications, which

　　intends to provide reference to the domestic development and research of laser-based

　　satellite technology. Conclusions and Prospects The laser inter-satellite link is developing vigorously. At

　　the same time, the mission requirements of the satellite network are complex and

　　diverse. For satellites of different orbits and mission types, the selection of the

　　communication system, wavelength, and access mode of the laser inter-satellite link

　　needs to be analyzed in detail according to each situation. The research of this paper

　　aims to provide some reference and reference for the design and optimization of laser

　　inter-satellite links in the future. It is expected that building a standardized, compatible, networked and commercialized laser inter-satellite link will help

　　maximize space resources and interconnection of satellite networks. Key words: laser intersatellite link; satellite laser communication; laser

　　communication terminal; satellite ranging

　　Funding projects: Natural Science Foundation of China (No.********)