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.

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
Online-Zugang:	Volltext
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