Attitude Control Design for Hypersonic Reentry Vehicles Subject to Control Direction Reversal via Sliding Mode Approach

Author:

Ding Yixin,Guo ZongyiORCID,Han Yonglin,Wang Jiaqi,Guo Jianguo,Liu Zequn,Zhao Jinlong

Funder

National Natural Science Foundation of China

Natural Science Foundation of Ningbo

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference27 articles.

1. Bao W, Wang X (2021) Prospect of airline-flight-mode aerospace transportation systems. Aircr. Eng. Aerosp. Technol 5(3):6

2. Zhang C, Wang Y, Ye L (2020) Summary of the technological development of overseas hypersonics in the past ten years. Tactical Missile Technol 6:81–86

3. Minnan P, Yang ZH, Sun MW, Huang J, Chen ZQ (2019) Attitude control synthesis of unstable hypersonic vehicle with aeroservoelastic effect. Sci Sinica Technol 49(7):15

4. Wang J, Liu L, Zhao T, Tang G (2016) Integrated guidance and control for hypersonic vehicles in dive phase with multiple constraints. Aerosp Sci Technol 53:103–115

5. Zhao S, Wang J, Xu H, Wang B (2023) Composite observer-based optimal attitude-tracking control with reinforcement learning for hypersonic vehicles. IEEE Trans Cybernet 53(2):913–926. https://doi.org/10.1109/TCYB.2022.3192871

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