[1] Zixuan Liang, Kenneth D. Mease. Precision guidance for Mars entry with a supersonic inflatable aerodynamic decelerator. Journal of Guidance, Control, and Dynamics, 2019, 42 (7): 1571-1578
[2] Zixuan Liang, Zhang Ren. Tentacle-based guidance for entry flight with no-fly zone constraint. Journal of Guidance, Control, and Dynamics, 2018, 41 (4): 991-1000
[3] Zixuan Liang, Jian Chen, Zhang Ren. Feasible zone for planetary entry vehicles. Aerospace Science and Technology, 2018, 79: 459-467
[4] Zixuan Liang, Zhang Ren, Qingdong Li. Evolved atmospheric entry corridor with safety factor. Acta Astronautica, 2018, 143: 82-91.
[5] Zixuan Liang, Siyuan Liu, Qingdong Li, Zhang Ren. Lateral entry guidance with no-fly zone constraint. Aerospace Science and Technology, 2017, 60: 39-47.
[6] Zixuan Liang, Qingdong Li, Zhang Ren. Virtual terminal-based adaptive predictor-corrector entry guidance. Journal of Aerospace Engineering, 2017, 30 (4): 04017013.
[7] Zixuan Liang, Zhang Ren, Qingdong Li, Jian Chen. Decoupled three-dimensional entry trajectory planning based on maneuver coefficient. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 231 (7): 1281–1292.
[8] Zixuan Liang, Guangfei Duan, Zhang Ren. Mars entry guidance based on an adaptive reference drag profile. Advances in Space Research, 2017, 60 (3): 692-701.
[9] Zixuan Liang, Qingdong Li, Zhang Ren. Waypoint constrained guidance for entry vehicles. Aerospace Science and Technology, 2016, 52: 52-61.
[10] Zixuan Liang, Qingdong Li, Zhang Ren. Onboard planning of constrained longitudinal trajectory for reusable launch vehicles in terminal area. Advances in Space Research, 2016, 57 (3): 742-753.
