Adaptive Control of Hypersonic Vehicles Using Observer-Based Nonlinear Dynamic Inversion
Author:
Affiliation:
1. Texas A&M University
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0843
Reference20 articles.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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2. Improved model reference‐based adaptive nonlinear dynamic inversion for fault‐tolerant flight control;International Journal of Robust and Nonlinear Control;2023-03
3. Tube-model predictive control based on sum of squares for hypersonic vehicle with state-dependent input constraints;Transactions of the Institute of Measurement and Control;2021-09-27
4. Nonlinear robust neuro-adaptive flight control for hypersonic vehicles with state constraints;Control Engineering Practice;2020-09
5. Stochastic precision analysis of hypersonic flight vehicle attitude control system in the presence of uncertainties;Systems Science & Control Engineering;2020-01-01
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