Attitude Determination by External Vectors in Airplane Free Spin Investigation
https://doi.org/10.17285/0869-7035.0040
Abstract
The article gives an overview of the methods for determining orientation angles from observations of external reference vectors. To maintain the observability of the kinematic parameters of the free-flying aircraft model motion in a vertical wind tun-nel, we analyzed the methods for determining the finite rotation vector using two, three or more vectors, known in a model body frame, as well as their derivatives. The methods to estimate the reliability of the calculated orientation angles are proposed. The method for estimating the radius of the free-flying model spin is considered.
About the Author
A. V. Vyalkov
Zhukovskiy Central Aerohydrodynamic Institute, Moscow region, Russia
Russian Federation
Russian Federation
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Review
For citations:
Vyalkov A.V. Attitude Determination by External Vectors in Airplane Free Spin Investigation. Giroskopiya i Navigatsiya. 2020;28(3):43-59. https://doi.org/10.17285/0869-7035.0040
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