Active Modeling Based Yaw Control of Unmanned Rotorcraft

Data publikacji: 10 mar 2014

Zakres stron: 380 - 399

Otrzymano: 10 paź 2013

Przyjęty: 02 lut 2014

DOI: https://doi.org/10.21307/ijssis-2017-661

Słowa kluczowe

Unmanned Rotorcraft, Active modeling technique, Model error, Kalman filter (KF)

© 2014 Yan Peng et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.