Design of Active Disturbance Rejection Attitude Controller for Vertical Launched Missile Based on Improved Particle Swarm Optimization
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6226-4_64
Reference16 articles.
1. Gui, H., Sun, R.S.: Improved backstepping control with adaptive estimation for nonlinear missile systems. J. Spacecr. Rocket. 59(1), 49–58 (2022). https://doi.org/10.2514/1.A34860
2. Lee, Y., Kim, Y., Moon, G.: Sliding-mode-based missile-integrated attitude control schemes considering velocity change. J. Guid. Control. Dyn. 39(3), 423–436 (2016). https://doi.org/10.2514/1.G001416
3. Ouyang, F.L., Li, L., Gong, C.L.: Research on the ejection attitude of vertical launching ship-borne rocket. Missiles Space Veh. 6, 50–54 (2020). https://doi.org/10.7654/j.issn.1004-7182.20200610
4. Xu, Q., Wang, Z.: Design of nonlinear active disturbance rejection acceleration tracking controller for gliding guided projectiles. Acta Armamentarii 38(7), 28–36 (2017). https://doi.org/10.3969/j.issn.1000-1093.2017.07.004
5. Li, H., Wang, L.: Design of active disturbance rejection attitude controller for vertical launched missile. In: Proceedings of the 40th Chinese Control Conference, pp. 7665–7670 (2021). https://doi.org/10.23919/CCC52363.2021.9549954
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