| Issue |
E3S Web Conf.
Volume 446, 2023
2nd International Conference on High-Speed Transport Development (HSTD 2023)
|
|
|---|---|---|
| Article Number | 06005 | |
| Number of page(s) | 15 | |
| Section | Mathematical Modeling | |
| DOI | https://doi.org/10.1051/e3sconf/202344606005 | |
| Published online | 10 November 2023 | |
Synthesis of Control Law Based on Nonlinear Dynamic Inversion for Supersonic Aircraft in Presence of Noise and Uncertainties
Moscow Aviation Institute, Moscow 125993, Russia
1 Corresponding author: gauravdhiman96@gmail.com
In this paper, the approach for synthesis of control law based on nonlinear dynamic inversion (NDI) via feedback linearization combined with Proportional–integral–derivative (PID) controller in outer loop to control supersonic aircraft in its most challenging flight task, i.e., landing in the presence of uncertainty in knowledge of model, measurement noise is developed. The results obtained demonstrate higher control accuracy, lower pilot workload compared to PI in tracking task of pitch angle of a supersonic passenger aircraft in presence of uncertainties, noise and in case of control surface faults.
© The Authors, published by EDP Sciences, 2023
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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