scholarly journals High-precision and fast-response laser power stabilization system for cold atom experiments

AIP Advances ◽  
2018 ◽  
Vol 8 (9) ◽  
pp. 095221 ◽  
Author(s):  
Qi-Xue Li ◽  
Shu-Hua Yan ◽  
Enlong Wang ◽  
Xu Zhang ◽  
Huankai Zhang
2021 ◽  
Vol 48 (1) ◽  
pp. 0101003
Author(s):  
欧阳鑫川 Ouyang Xinchuan ◽  
杨博文 Yang Bowen ◽  
万金银 Wan Jinyin ◽  
肖玲 Xiao Ling ◽  
成华东 Cheng Huadong

2016 ◽  
Vol 9 (2) ◽  
pp. 263-269 ◽  
Author(s):  
苗少峰 MIAO Shao-feng ◽  
李晨旭 LI Chen-xu ◽  
高 苗 GAO Miao ◽  
邵晓鹏 SHAO Xiao-peng ◽  
史学舜 SHI Xue-shun ◽  
...  

2016 ◽  
Vol 36 (8) ◽  
pp. 0814004
Author(s):  
李琳 Li Lin ◽  
刘鹏 Liu Peng ◽  
吉经纬 Ji Jingwei ◽  
成华东 Cheng Huadong ◽  
刘亮 Liu Liang ◽  
...  

2020 ◽  
Vol 9 (5) ◽  
pp. 221-225
Author(s):  
Ravi Kumar ◽  
Ana Rakonjac

AbstractAtom interferometry is one of the most promising technologies for high precision measurements. It has the potential to revolutionise many different sectors, such as navigation and positioning, resource exploration, geophysical studies, and fundamental physics. After decades of research in the field of cold atoms, the technology has reached a stage where commercialisation of cold atom interferometers has become possible. This article describes recent developments, challenges, and prospects for quantum sensors for inertial sensing based on cold atom interferometry techniques.


2021 ◽  
Vol 22 (7) ◽  
pp. 365-373
Author(s):  
Quang Thong Do

The proportional guidance method-based missile homing systems (MHS) have been widely used the real-world environments. In these systems, in order to destroy the targets at different altitudes, a normal acceleration stabilization system (NASS) is often utilized. Therefore, the MHS are complex and the synthesis of these systems are a complex task. However, it is necessary to synthesize NASS during the synthesis of the MHS. To simplify the synthesis process, a linear model of the NASS is used. In addition, we make use of the available commands in Control System Toolbox in MATLAB. Because the Toolbox has the commands to describe the transfer function, determine the stability gain margin, and the values of the transient respond of the linear automatic systems. Thus, this article presents two methods for synthesizing the missile homing systems, including (i) a method for synthesizing the MHS while ensuring the permissible stability gain margin of the NASS, and (ii) a method for synthesizing the MHS while ensuring the permissible stability margin of the NASS by overshoot. These techniques are very easy to implement using MATLAB commands. The synthesis of the proposed MHS is carried out by the parametric optimization method. To validate the performance of the proposed techniques, we compare them withthe MHS synthesized by ensuring the stability margin of the NASS bythe oscillation index. The results show that, two our proposed methods and the existing method provide the same results in terms of high-precision. Nevertheless, the proposed methods are simple and faster than the conventional method. The article also investigates the effect of gravity, longitudinal acceleration of the rocket, andblinding of the homing head on the accuracy of the synthesized MHS. The results illustrate that they have a little effect on its accuracy.


2021 ◽  
Author(s):  
Xia Wang ◽  
Xunmin Zhu ◽  
Nan Li ◽  
Mengzhu Hu ◽  
Wenqiang Li ◽  
...  

Author(s):  
Frederic Cleva ◽  
Jean-Pierre Coulon ◽  
Li Wei Wei ◽  
Margherita Turconi ◽  
Mourad Merzougui ◽  
...  

2010 ◽  
Vol 37 (1) ◽  
pp. 82-86
Author(s):  
江晓 Jiang Xiao ◽  
张晨 Zhang Chen ◽  
蔡文奇 Cai Wenqi ◽  
金革 Jin Ge

2014 ◽  
Vol 898 ◽  
pp. 910-913
Author(s):  
Hui Can Lin ◽  
Tao Guo ◽  
Yu Shi ◽  
Yang Liu ◽  
Zi Jing Zhong

Aircraft control, the training process to locate the aircraft attitude and heading information monitoring requires high-precision gesture as a feedback input, application STM32F103T8 processor design a combination of positioning technology and attitude sensor acquisition system. Measurement module with low power consumption, fast response and high accuracy, the use of high precision MEMS devices with 32-bit processors STM32F103T8 good data processing capabilities. For sensor characteristics, extended Kalman filter algorithm is designed based on dual quaternion vector correction method, enhanced anti-jamming capability; characteristics of complex electromagnetic environment, an improved forward linear prediction filtering method, processing the received GPS data, improving positioning accuracy. The results show that the proposed method effectively suppress noise, gesture detection, accurate and fast.


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