Patents by Inventor Yoshimi OHSHIMA

Yoshimi OHSHIMA 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: 11061143
    Abstract: In a satellite navigation system a navigation terminal continuously receives navigation signals from navigation satellites and continuously implements navigation calculations, thereby obtaining navigation calculation results, and executes in parallel: using clock offset values determined through the navigation calculations, calculates, in real time, changes in difference between time differences with regard to difference between time differences, which are differences between a clock offset value and a standard deviation value, which is the value of the standard deviation of fluctuation amounts of the clock offset values; determines, in real time, two navigation precision indices of the calculated navigation calculation results on the basis of each change in the calculated difference between time differences and standard deviation value; associates, in real time, the determined two navigation precision indices with the calculated navigation calculation results; and outputs, in real time, the navigation calcul
    Type: Grant
    Filed: March 17, 2017
    Date of Patent: July 13, 2021
    Assignee: NEC CORPORATION
    Inventors: Hiroshi Soga, Yoshimi Ohshima, Tomoya Osawa, Aki Taniyama, Aki Sakamoto
  • Patent number: 10564295
    Abstract: Provided is a positioning terminal of a global navigation satellite system configured to: receive a plurality of navigation signals and an augmentation signal from a plurality of navigation satellites and an augmentation satellite; acquire, in a process of causing each value of error causes including an ambiguity to converge through a plurality of times of observation to enhance an accuracy of positioning through continuous observation, each value of a position of the positioning terminal recorded in advance in a storage area to calculate each value of the error cause, and use the calculated each value as an initial value and/or one value to be added for the continuous observation to cause each value of the error cause to converge; and successively perform positioning calculation.
    Type: Grant
    Filed: December 24, 2014
    Date of Patent: February 18, 2020
    Assignee: NEC CORPORATION
    Inventors: Hiroshi Soga, Yoshimi Ohshima, Tomoya Osawa, Aki Taniyama
  • Publication number: 20190101653
    Abstract: In a satellite navigation system a navigation terminal continuously receives navigation signals from navigation satellites and continuously implements navigation calculations, thereby obtaining navigation calculation results, and executes in parallel: using clock offset values determined through the navigation calculations, calculates, in real time, changes in difference between time differences with regard to difference between time differences, which are differences between a clock offset value and a standard deviation value, which is the value of the standard deviation of fluctuation amounts of the clock offset values; determines, in real time, two navigation precision indices of the calculated navigation calculation results on the basis of each change in the calculated difference between time differences and standard deviation value; associates, in real time, the determined two navigation precision indices with the calculated navigation calculation results; and outputs, in real time, the navigation calcul
    Type: Application
    Filed: March 17, 2017
    Publication date: April 4, 2019
    Applicant: NEC Corporation
    Inventors: Hiroshi SOGA, Yoshimi OHSHIMA, Tomoya OSAWA, Aki TANIYAMA, Aki SAKAMOTO
  • Publication number: 20170038475
    Abstract: Provided is a positioning terminal of a global navigation satellite system configured to: receive a plurality of navigation signals and an augmentation signal from a plurality of navigation satellites and an augmentation satellite; acquire, in a process of causing each value of error causes including an ambiguity to converge through a plurality of times of observation to enhance an accuracy of positioning through continuous observation, each value of a position of the positioning terminal recorded in advance in a storage area to calculate each value of the error cause, and use the calculated each value as an initial value and/or one value to be added for the continuous observation to cause each value of the error cause to converge; and successively perform positioning calculation.
    Type: Application
    Filed: December 24, 2014
    Publication date: February 9, 2017
    Inventors: Hiroshi SOGA, Yoshimi OHSHIMA, Tomoya OSAWA, Aki TANIYAMA