Email this article About the Efficient Scheme of Initial Attitude Estimation Using Low Accuracy Micro-Electro-Mechanical Sensors
- Authors: Gainutdinova T.Y.1, Gainutdinova A.V.2, Gainutdinov V.G.2
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Affiliations:
- Kazan (Volga region) Federal University
- Tupolev Kazan National Research Technical University
- Issue: Vol 62, No 3 (2019)
- Pages: 387-393
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/231021
- DOI: https://doi.org/10.3103/S106879981903005X
- ID: 231021
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Abstract
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.
About the authors
T. Yu. Gainutdinova
Kazan (Volga region) Federal University
Author for correspondence.
Email: tgainut@mail.ru
Russian Federation, ul. Kremlevskaya 18, Kazan, 420008 Tatarstan
A. V. Gainutdinova
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. G. Gainutdinov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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