Attitude/Parameter Coupling Modeling and Sliding Mode Control System Design for Hyper-Glide Vehicle

Author:

Guo Dong,Gong Min,Gao Feng,Dong Xiwang,Ren Zhang

Publisher

Springer Singapore

Reference8 articles.

1. Huaping, Z., Chongwen, J.: Review on HTV-2 of hypersonic technology verification aircraft. Aerodyn. Missile J. 6, 7–13 (2013)

2. Wenjie, L., Wen, N.: DARPA discloses the conclusion of the second test flight evaluation of HTV-2. Aerodyn. Missile J. 9, 30–32 (2012)

3. Georgie, J., Valasek, J.: Evaluation of longitudinal desired dynamics for dynamic-inversion controlled generic reentry vehicles. J. Guidance Control Dyn. 26(5), 811–819 (2003)

4. Chen, B., Zhang, R., et al.: Dynamic inversion control for RLV reentry attitude based on fuzzy-neural disturbance observer. J. Central South Univ. (Sci. Technol.) 44(S1), 58–62 (2013)

5. Guoqing, W., Jianguo, G., et al.: Adaptive sliding mode attitude control system design for reentry vehicle. Flight Dyn. 37(03), 74–78 (2019)

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