Initial fine alignment based on self‐contained measurement in erection manoeuvre-Reference-Cited by-同舟云学术

Initial fine alignment based on self‐contained measurement in erection manoeuvre

Published:2018-05 Issue:3 Volume:12 Page:375-381
ISSN:1751-8830
Container-title:IET Science, Measurement & Technology
language:en
Short-container-title:IET Science, Measurement & Technology

Author:

Li Jianli¹²^ORCID,Li Yiqi¹,Zhai Fengguang¹

Affiliation:

1. School of Instrument Science and Opto‐electronic EngineeringBeijing University of Aeronautics and AstronauticsBeijingPeople's Republic of China

2. The National Key Laboratory of Satellite Navigation System and Equipment TechnologyThe 54th Research Institute of China Electronics Technology Group CorporationShijiazhuangPeople's Republic of China

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Atomic and Molecular Physics, and Optics

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-smt.2017.0349

Reference22 articles.

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2. A miniature integrated navigation system for rotary‐wing unmanned aerial vehicles;Xu Y.;Int. J. Aerosp. Eng.,2014

3. Initial Alignment by Attitude Estimation for Strapdown Inertial Navigation Systems

4. Strapdown inertial navigation system alignment based on marginalised unscented Kalman filter

5. An improved initial alignment method for rocket navigation systems;Cheng X.H.;J. Navig.,2013

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