About the Efficient Scheme of Initial Attitude Estimation Using Low Accuracy Micro-Electro-Mechanical Sensors

A solution of initial attitude estimation is considered for the UAV with an inertial navigation system including a standard set of three-degree micro-electro-mechanical gyroscopic angular velocity sensors, accelerometers, and magnetometers.

Saved in:
Bibliographic Details
Published in:Russian aeronautics 2019-07, Vol.62 (3), p.387-393
Main Authors: Gainutdinova, T. Yu, Gainutdinova, A. V., Gainutdinov, V. G.
Format: Article
Language:English
Subjects:
Accelerometers
Angular velocity
Attitudes
Automotive Engineering
Engineering
Flight Dynamics and Control of Flight Vehicles
Inertial navigation
Navigation systems
Sensors
Unmanned aerial vehicles
Citations: Items that this one cites
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:A solution of initial attitude estimation is considered for the UAV with an inertial navigation system including a standard set of three-degree micro-electro-mechanical gyroscopic angular velocity sensors, accelerometers, and magnetometers.
ISSN:1068-7998
1934-7901
DOI:10.3103/S106879981903005X