Modified deep deterministic policy gradient based on active disturbance rejection control for hypersonic vehicles
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
Artificial Intelligence,Software
Link
https://link.springer.com/content/pdf/10.1007/s00521-023-09302-5.pdf
Reference45 articles.
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2. Wang Y, Yang X, Yan H (2019) Reliable fuzzy tracking control of near-space hypersonic vehicle using aperiodic measurement information. IEEE Transact Ind Electron 66(12):9439–9447
3. Tang S, Hu C (2017) Design, preparation and properties of carbon fiber reinforced ultra-high temperature ceramic composites for aerospace applications: a review. J Mater Sci Technol 33(2):117–130
4. Zhang H, Wang H, Li N, Yu Y, Su Z, Liu Y (2020) Time-optimal memetic whale optimization algorithm for hypersonic vehicle reentry trajectory optimization with no-fly zones. Neural Comput Appl 32:2735–2749
5. Ding Y, Yue X, Chen G, Si J (2022) Review of control and guidance technology on hypersonic vehicle. Chin J Aeronaut 35(7):1–18
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