Patents by Inventor Luzhao CHEN

Luzhao CHEN 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).

  • Patent number: 11506811
    Abstract: A magnetic compensation method based on an aeromagnetic compensation error model includes: acquiring an upper limit of an error of a magnetic noise caused by both an environmental background field in an exploration area and an aeromagnetic flight platform, by using the aeromagnetic compensation error model, before an actual flight; determining, according to the upper limit, whether the environmental background field and the aeromagnetic flight platform are suitable for the actual flight, and if so, performing a calibration flight to acquire a compensation coefficient; and acquiring data of an attitude term by performing the actual flight, calculating an interference magnetic field by the data of the attitude term and the compensation coefficient, and performing magnetic compensation.
    Type: Grant
    Filed: September 30, 2017
    Date of Patent: November 22, 2022
    Assignee: Aerospace Information Research Institute, Chinese Academy of Sciences
    Inventors: Qunying Zhang, Peilin Wu, Luzhao Chen, Guangyou Fang, Wanhua Zhu
  • Publication number: 20200301040
    Abstract: The present disclosure discloses a magnetic compensation method for performance quality assessment by using an aeromagnetic compensation error model, comprising: acquiring an upper limit of an error of a magnetic noise by using the aeromagnetic compensation error model, before an aeromagnetic flight, wherein the magnetic noise is caused by both an environmental background field in an exploration area and an aeromagnetic flight platform; determining, according to the upper limit of the error of the magnetic noise, whether the environmental background field and the aeromagnetic flight platform are suitable for an aeromagnetic survey flight, and if so, performing a calibration flight to acquire a compensation coefficient; and acquiring data of an attitude term by performing an actual flight, calculating an interference magnetic field by the data of the attitude term and the compensation coefficient acquired during the calibration flight, and performing magnetic compensation.
    Type: Application
    Filed: September 30, 2017
    Publication date: September 24, 2020
    Inventors: Qunying ZHANG, Peilin WU, Luzhao CHEN, Guangyou FANG, Wanhua ZHU