A Three-Dimensional Terminal Guidance Law for Unpowered Gliding Vehicles Considering Dynamic Pressure and Impact Angle Constraints

Author:

Meng Wu,Fenghua Chi,Shichao Tian,Zheng Qi,Cong Xu

Publisher

Springer Singapore

Reference12 articles.

1. Zhao, Y., Li, P., Liu, J., et al.: Finite-time sliding mode control based 3D guidance law with impact angle constraint. J. Beijing Univ. Aeron. Astronaut. 44(2), 273–279 (2018). (in Chinese)

2. Xiaodong, Y., Zhi, W.: Three-dimensional trajectory planning method for hypersonic glide vehicles. J. Beijing Univ. Aeron. Astronaut. 33(7), 669–674 (2013). (in Chinese)

3. Siyuan, Chen., Qunli, Xia, Qiang, Li: Hypersonic glide guidance method of reentry vehicle for time-sensitive target. J. Astronaut. 37(8), 984–991 (2016). (in Chinese)

4. Liang, P., Xie, Y., Peng, S., Xu, L., Yuan, T.: A survey of gliding guidance methods for hypersonic vehicles. J. Natl. Univ. Defense Technol. 39(3), 15–22 (2017). (in Chinese)

5. Zhi, W., Shuo, T., Xiaodong, Y.: Constraint prediction correction reentry guidance of hypersonic gliding vehicle. Flight Dyn. 30, 175–180 (2012). (in Chinese)

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