Coordinated Reentry Guidance with A* and Deep Reinforcement Learning for Hypersonic Morphing Vehicles Under Multiple No-Fly Zones
Hypersonic morphing vehicles (HMVs), renowned for their adaptive structural reconfiguration and cross-domain maneuverability, confront formidable reentry guidance challenges under multiple no-fly zones, stringent path constraints, and nonlinear dynamics exacerbated by morphing-induced aerodynamic uncertainties. To address these issues, this study proposes a hierarchical framework integrating an A-based energy-optimal waypoint planner, a deep deterministic policy gradient (DDPG)-driven morphing policy network, and a quasi-equilibrium glide condition (QEGC) guidance law with continuous sliding mode control. The A* algorithm generates heuristic trajectories circumventing no-fly zones, reducing the evaluation function by 6.2% compared to greedy methods, while DDPG optimizes sweep angles to minimize velocity loss and terminal errors (0.09 km position, 0.01 m/s velocity). The QEGC law ensures robust longitudinal-lateral tracking via smooth hyperbolic tangent switching. Simulations demonstrate generalization across diverse targets (terminal errors < 0.24 km) and robustness under Monte Carlo deviations (0.263 ± 0.184 km range, −12.7 ± 42.93 m/s velocity). This work bridges global trajectory planning with real-time morphing adaptation, advancing intelligent HMV control. Future research will extend this framework to ascent/dive phases and optimize its computational efficiency for onboard deployment.
Authors
- Weile Xu (ORCID: https://orcid.org/0000-0002-2177-2996)
- Cunyu Bao (ORCID: https://orcid.org/0000-0001-5925-1291)
- Guojian Tang (ORCID: https://orcid.org/0000-0001-5198-5477)
- Wen Yao (ORCID: https://orcid.org/0000-0001-5224-9834)
- Xingchen Li (ORCID: https://orcid.org/0000-0002-2786-5392)
Institutions
- National University of Defense Technology (CN)
- Chinese People's Liberation Army (CN)
- Air Force Harbin Flying College
- Beihang University (CN)
Publication Details
- Journal
- Aerospace
- Published
- 2025-06-30
- DOI
- https://doi.org/10.3390/aerospace12070591
- Citations
- 2
- Primary Topic
- Computational Fluid Dynamics and Aerodynamics
- Type
- article
- Field-Weighted Citation Impact
- 2.67