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

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.

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Bibliographische Detailangaben
Veröffentlicht in:Russian aeronautics 2019-07, Vol.62 (3), p.387-393
Hauptverfasser: Gainutdinova, T. Yu, Gainutdinova, A. V., Gainutdinov, V. G.
Format: Artikel
Sprache:eng
Schlagworte:
Accelerometers
Angular velocity
Attitudes
Automotive Engineering
Engineering
Flight Dynamics and Control of Flight Vehicles
Inertial navigation
Navigation systems
Sensors
Unmanned aerial vehicles
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Beschreibung
Zusammenfassung: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