In-flight initial alignment for small UAV MEMS-based navigation via adaptive unscented Kalman filtering approach-Reference-Cited by-同舟云学术

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In-flight initial alignment for small UAV MEMS-based navigation via adaptive unscented Kalman filtering approach

Published:2017-02 Issue: Volume:61 Page:73-84
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Dingjie,Lv Hanfeng,Wu Jie

Funder

National University of Defense Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference33 articles.

1. Unmanned aerial vehicles: an overview;de Fatima Bento;InsideGNSS,2008

2. Autonomous navigation and landing tasks for fixed wing small unmanned aerial vehicles;Kurnaz;Acta Polytech. Hung.,2010

3. Principle of GNSS, Inertial, and Multisensor Integrated Navigation System;Groves,2008

4. An integrated GPS/MEMS-IMU navigation system for an autonomous helicopter;Wendel;Aerosp. Sci. Technol.,2006

5. Novel in-flight coarse alignment of low-cost strapdown inertial navigation system for unmanned aerial vehicle applications;Wang;Trans. Jpn. Soc. Aeronaut. Space Sci.,2016

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