Inter-relationship between approximate dynamic inversion and MRAC augmented with proportional-integral controller
Author:
Affiliation:
1. Department of Applied Electronics and Instrumentation Engineering, Bankura Unnayani Institute of Engineering, Bankura, India
2. Instrumentation Engineering, Department of Applied Physics, University of Calcutta, Kolkata, India
Publisher
Informa UK Limited
Subject
Artificial Intelligence,Control and Optimization,Computer Networks and Communications,Human-Computer Interaction,Information Systems,Signal Processing,Control and Systems Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/23307706.2022.2076162
Reference18 articles.
1. Agile Spacecraft Attitude Control: an Incremental Nonlinear Dynamic Inversion Approach
2. PI(D) tuning for Flight Control Systems via Incremental Nonlinear Dynamic Inversion
3. Self-Tuning PID Controllers Based on Dynamics Inversion Method
4. Ducard, G. & Geering, H. P. (2008). Stability analysis of a dynamic inversion based pitch rate controller for an unmanned aircraft. 2008 IEEE/RSJ International Conference on Intelligent Robots and Systems (pp. 360–366). https://doi.org/10.1109/IROS.2008.4651117
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