Systems Engineering and Electronics ›› 2026, Vol. 48 ›› Issue (2): 694-704.doi: 10.12305/j.issn.1001-506X.2026.02.29

• Guidance, Navigation and Control • Previous Articles     Next Articles

Attitude control of hypersonic vehicle based on dual-dynamic PPO algorithm

Xu WANG, Guangbin CAI, Xiaoya YU, Ziqi YE, Bin SHAN   

  1. School of Missile Engineering,Rocket Force Engineering University,Xi’an 710025,China
  • Received:2025-01-15 Revised:2025-03-06 Online:2025-06-10 Published:2025-06-10
  • Contact: Guangbin CAI

Abstract:

To address the strong nonlinearities and significant uncertainties in hypersonic vehicle attitude control, as well as the limitations of traditional reinforcement learning algorithms in training convergence and control accuracy under multiple control requirements, a dual-dynamic adaptive proximal policy optimization (PPO) algorithm is proposed. The algorithm balances control precision and actuator protection through a soft dynamic clipping mechanism and a policy-driven entropy adjustment strategy. An integrated simulation environment incorporating aerodynamic characteristics and actuator dynamic characteristics is subsequently established. By integrating proportional-integral-derivative control principles, the state observation space is optimally redesigned. Simulation results demonstrate that compared with the baseline PPO algorithm, the proposed method improves convergence speed by 22% while significantly enhancing both control accuracy and action smoothness. Under different flight conditions, this method exhibits excellent strategic adaptability and robustness, and effectively improves the attitude control performance of the hypersonic vehicle.

Key words: hypersonic vehicle, intelligent control, deep reinforcement learning, proximal policy optimization (PPO), dynamic adaptive mechanism

CLC Number: 

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