A GNSS/IMU/Vision Ultra-Tightly Integrated Navigation System for Low Altitude Aircraft-Reference-Cited by-同舟云学术

A GNSS/IMU/Vision Ultra-Tightly Integrated Navigation System for Low Altitude Aircraft

Published:2022-06-15 Issue:12 Volume:22 Page:11857-11864
ISSN:1530-437X
Container-title:IEEE Sensors Journal
language:
Short-container-title:IEEE Sensors J.

Author:

Zuo Zhaoyang¹^ORCID,Yang Bo²^ORCID,Li Ze¹,Zhang Tianhao¹

Affiliation:

1. School of Mechanical Engineering, Xijing University, Xi’an, China

2. Control Engineering Department, Xi’an Research Institute of High Technology, Xi’an, China

Funder

Shaanxi Science and Technology Plan Project

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Instrumentation

Link

http://xplorestaging.ieee.org/ielx7/7361/9795939/09759432.pdf?arnumber=9759432

Reference15 articles.

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3. A visual/inertial integrated navigation algorithm based on improved Kalman filter;liu;Navigation Positioning & Timing[J],2017

4. Optimized design of thenavigation filter in ultra-tight GPS/INS integratio;zhang;Trans Beijing Inst Technol,2018

5. Transitional mode manipulation strategy of tilt tri-rotor UAVs based on fuzzy control;zhang;Electron Opt Control,2018

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