Lie Group Quaternion Attitude-Reconstruction of Quadrotor UAV
Author:
Publisher
Springer Nature Switzerland
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-38299-4_1
Reference12 articles.
1. Hoffman, D., Rehan, M., MacKunis, W., Reyhanoglu, M.: Quaternion-based robust trajectory tracking control of a quadrotor hover system. Int. J. Control Autom. Syst. 16, 1–10 (2018)
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3. Hartley, R., Trumpf, J., Dai, Y., Li, H.: Rotation averaging. Int. J. Comput. Vision 103, 267–305 (2013)
4. Terze, Z., Müller, A., Zlatar, D.: Singularity-free time integration of rotational quaternions using non-redundant ordinary differential equations. Multibody Sys.Dyn. 38(3), 201–225 (2016). https://doi.org/10.1007/s11044-016-9518-7
5. Terze, Z., Zlatar, D., Pandža, V.: Aircraft attitude reconstruction via novel quaternion-integration procedure. Aerosp. Sci. Technol. 97, 105617 (2020)
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