Hongyu Zhou
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Hongyu Zhou has a total of 10 co-authors. Here are the top co-authors by number of shared publications:
Xiaogang Wang
6 shared publicationsNaigang Cui
4 shared publications- Xun Li
School of Astronautics, Harbin Institute of Technology, Harbin, China
3 shared publications Yuliang Bai
2 shared publicationsBing Bai
1 shared publicationN.G. Cui
Harbin Institute of Technology, Harbin, China
1 shared publication
Latest Publications
- Top Cited Papers
- 9 May 2025
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Aerospace and Electronic Systems
- Vol. PP (00189251) , 1-18
Trajectory Planning for Reusable Launch Vehicle with Multisolution-based Maximum Entropy Reinforcement Learning
Online trajectory planning is very important to the reusable launch vehicle (RLV) in emergency return cases. However, computing the optimal trajectory instantaneously is challenging, particularly when there is complicated nonlinear coupling between strict constraints, load-thermal factors, and dynamics. To cope with this problem, this paper begins with a return profile that easily satisfies strict constraints. Moreover, to mitigate the nonlinear coupling and computational cost for online trajectory planning, we propose two types of analytical models for return trajectories based on the quasi-equilibrium glide condition (QEGC) in the time-domain and another type of analytical model under phugoid oscillation condition in the Laplace frequency domain. Thus, the proposed models depict the return trajectory in both the time and frequency domains, breaking the limitations on return scenario. By contrast, most of existing algorithms are limited to either QEGC or jumping flight. The proposed analytical models also take consideration of different aerodynamic expressions and assumptions, which makes our method adaptive to various return scenarios, flight states, and computational efficiency requirements. Moreover, we devise the maximum entropy strategy and adaptive noises for the reinforcement learning agent training and accomplish online trajectory planning by using the trained optimal agent. In the long period of planning, the agent determines the most appropriate return profile and type of analytical model based on the real-time return status. In the short period of planning, the agent computes the three-dimensional trajectory based on the selected profile and model via instantaneous decision. The numerical simulation validates the method performances: the training exhibits robust and the agent has adaptively selected the analytical model with the best accuracy.
- 9 May 2025
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Aerospace and Electronic Systems
- Vol. PP (00189251) , 1-18
Top Cited PapersTrajectory Planning for Reusable Launch Vehicle with Multisolution-based Maximum Entropy Reinforcement Learning
Online trajectory planning is very important to the reusable launch vehicle (RLV) in emergency return cases. However, computing the optimal trajectory instantaneously is challenging, particularly when there is complicated nonlinear coupling between strict constraints, load-thermal factors, and dynamics. To cope with this problem, this paper begins with a return profile that easily satisfies strict constraints. Moreover, to mitigate the nonlinear coupling and computational cost for online trajectory planning, we propose two types of analytical models for return trajectories based on the quasi-equilibrium glide condition (QEGC) in the time-domain and another type of analytical model under phugoid oscillation condition in the Laplace frequency domain. Thus, the proposed models depict the return trajectory in both the time and frequency domains, breaking the limitations on return scenario. By contrast, most of existing algorithms are limited to either QEGC or jumping flight. The proposed analytical models also take consideration of different aerodynamic expressions and assumptions, which makes our method adaptive to various return scenarios, flight states, and computational efficiency requirements. Moreover, we devise the maximum entropy strategy and adaptive noises for the reinforcement learning agent training and accomplish online trajectory planning by using the trained optimal agent. In the long period of planning, the agent determines the most appropriate return profile and type of analytical model based on the real-time return status. In the short period of planning, the agent computes the three-dimensional trajectory based on the selected profile and model via instantaneous decision. The numerical simulation validates the method performances: the training exhibits robust and the agent has adaptively selected the analytical model with the best accuracy.
- 20 July 2024
- Published by Elsevier in Aerospace Science and Technology
- Vol. 153
Entry guidance for spatial no-fly zones avoidance via model-based reinforcement learning
- 20 July 2024
- Published by Elsevier in Aerospace Science and Technology
- Vol. 153
Entry guidance for spatial no-fly zones avoidance via model-based reinforcement learning
- Open Access
- 6 March 2024
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 37 (5) , 441-461
A novel evasion guidance for hypersonic morphing vehicle via intelligent maneuver strategy
- 6 March 2024
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 37 (5) , 441-461
Open AccessA novel evasion guidance for hypersonic morphing vehicle via intelligent maneuver strategy
- 13 December 2022
- Published by Elsevier in Aerospace Science and Technology
- Vol. 132
Optimal guidance for hypersonic vehicle using analytical solutions and an intelligent reversal strategy
- 13 December 2022
- Published by Elsevier in Aerospace Science and Technology
- Vol. 132
Optimal guidance for hypersonic vehicle using analytical solutions and an intelligent reversal strategy
- 1 March 2020
- Published by Elsevier in Aerospace Science and Technology
- Vol. 98
Glide guidance for reusable launch vehicles using analytical dynamics
- 1 March 2020
- Published by Elsevier in Aerospace Science and Technology
- Vol. 98
Glide guidance for reusable launch vehicles using analytical dynamics
- 1 November 2019
- Published by Elsevier in Acta Astronautica
- Vol. 164, 376-386
Glide trajectory optimization for hypersonic vehicles via dynamic pressure control
- 1 November 2019
- Published by Elsevier in Acta Astronautica
- Vol. 164, 376-386
Glide trajectory optimization for hypersonic vehicles via dynamic pressure control
- 1 July 2018
- Published by Elsevier in Aerospace Science and Technology
- Vol. 78, 205-213
Reentry guidance with constrained impact for hypersonic weapon by novel particle swarm optimization
- 1 July 2018
- Published by Elsevier in Aerospace Science and Technology
- Vol. 78, 205-213
Reentry guidance with constrained impact for hypersonic weapon by novel particle swarm optimization
- 1 November 2017
- Published by Elsevier in Acta Astronautica
- Vol. 140, 156-165
Ascent phase trajectory optimization for vehicle with multi-combined cycle engine based on improved particle swarm optimization
- 1 November 2017
- Published by Elsevier in Acta Astronautica
- Vol. 140, 156-165
Ascent phase trajectory optimization for vehicle with multi-combined cycle engine based on improved particle swarm optimization