Patents by Inventor Mingxue SHAO

Mingxue SHAO has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • High-precision magnetic suspension accelerometer
    Patent number: 10444257
    Abstract: A high-precision magnetic suspension accelerometer for measuring the linear acceleration of a spacecraft is provided, comprising a magnetically shielded vacuum chamber system, a magnetic displacement sensing system, a magnetic suspension control system and a small magnetic proof mass. A optical coherence displacement detection technique is utilized for precisely measuring the position and the posture of the small magnetic proof mass in real time, and a magnetic suspension control technique is utilized for precisely controlling the position and the posture of the small magnetic proof mass to be brought back to the origin, so as to keep the small magnetic proof mass in the center of the systemic inner chamber. When the spacecraft is subject to a non-conservative force, the magnitude and direction of the acceleration can be precisely measured via the measurement of currents in the position control coils due to the acceleration of the spacecraft proportional to the currents of the position control coils.
    Type: Grant
    Filed: February 17, 2017
    Date of Patent: October 15, 2019
    Assignee: CHINA THREE GORGES UNIVERSITY
    Inventors: Liqing Pan, Xianwei Yang, Zhihui Luo, Hua Zhao, Mingxue Shao, Qiongying Ren, Chao Tan, Min Liu, Chao Wang, Chao Zhang, Sheng Zheng, Hongguang Piao, Guangduo Lu, Yunli Xu, Xiufeng Huang
  • HIGH-PRECISION MAGNETIC SUSPENSION ACCELEROMETER
    Publication number: 20170242050
    Abstract: A high-precision magnetic suspension accelerometer for measuring the linear acceleration of a spacecraft is provided, comprising a magnetically shielded vacuum chamber system, a magnetic displacement sensing system, a magnetic suspension control system and a small magnetic proof mass. A optical coherence displacement detection technique is utilized for precisely measuring the position and the posture of the small magnetic proof mass in real time, and a magnetic suspension control technique is utilized for precisely controlling the position and the posture of the small magnetic proof mass to be brought back to the origin, so as to keep the small magnetic proof mass in the center of the systemic inner chamber. When the spacecraft is subject to a non-conservative force, the magnitude and direction of the acceleration can be precisely measured via the measurement of currents in the position control coils due to the acceleration of the spacecraft proportional to the currents of the position control coils.
    Type: Application
    Filed: February 17, 2017
    Publication date: August 24, 2017
    Applicant: CHINA THREE GORGES UNIVERSITY
    Inventors: Liqing PAN, Xianwei YANG, Zhihui LUO, Hua ZHAO, Mingxue SHAO, Qiongying REN, Chao TAN, Min LIU, Chao WANG, Chao ZHANG, Sheng ZHENG, Hongguang PIAO, Guangduo LU, Yunli XU, Xiufeng HUANG