Invention Grant
- Patent Title: Method for initial alignment of an inertial navigation apparatus
-
Application No.: US15542442Application Date: 2016-07-04
-
Publication No.: US10670424B2Publication Date: 2020-06-02
- Inventor: Qiang Ren , Jiejun Wang , Xuefeng Shen , Lilong Wei , Guiyan Cui
- Applicant: SHANGHAI HUACE NAVIGATION TECHNOLOGY LTD
- Applicant Address: CN Shanghai
- Assignee: SHANGHAI HUACE NAVIGATION TECHNOLOGY LTD
- Current Assignee: SHANGHAI HUACE NAVIGATION TECHNOLOGY LTD
- Current Assignee Address: CN Shanghai
- Agency: Bayramoglu Law Office LLC
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@5aa6041a
- International Application: PCT/CN2016/088343 WO 20160704
- International Announcement: WO2017/063388 WO 20170420
- Main IPC: G01C25/00
- IPC: G01C25/00 ; G01C21/16

Abstract:
A method for initial alignment of an inertial navigation apparatus, comprising the following steps: providing an apparatus loaded with a sensor, and preprocessing the sensor; carrying out relative alignment to calculate an installation error angle of the sensor; carrying out absolute alignment to calculate an installation attitude angle error of the sensor to increase an accuracy of an error attitude angle calculated during the relative alignment. The relative alignment process calculates a relative error attitude angle, the relative error attitude angle being used as the initial value for attitude error in a stat vector in the absolute alignment process, thereby accelerating convergence of the Kalman filter. Alignment precision is further enhanced by the absolute alignment process.
Public/Granted literature
- US20180274940A1 A METHOD FOR INITIAL ALIGNMENT OF AN INERTIAL NAVIGATION APPARATUS Public/Granted day:2018-09-27
Information query