Optimizing trajectory tracking control for hypersonic flight vehicles via ADDHP
- PMID: 40841259
- DOI: 10.1016/j.isatra.2025.08.017
Optimizing trajectory tracking control for hypersonic flight vehicles via ADDHP
Abstract
This article proposes an intelligent hybrid control strategy for hypersonic flight vehicles (HFVs) that integrates sliding mode control (SMC) with actor-dependent dual heuristic programming (ADDHP) to address trajectory tracking challenges. An SMC baseline controller is first developed to ensure stable tracking with model uncertainties. Additionally, a novel angle of attack (AOA) protection mechanism is designed, which maintains the AOA within constraint boundaries by generating smooth modifying signals. Furthermore, multiple ADDHP-based optimal compensators are then implemented in the velocity and altitude subsystems. These model-free compensators dynamically optimize control performance through error-driven learning, significantly improving tracking accuracy and adaptability in complex environments. Lyapunov stability analysis proves the convergence of both SMC and ADDHP. The effectiveness and superiority of the proposed strategy are validated through comparative simulations.
Keywords: Actor-dependent dual heuristic programming; Angle of attack constraint; Hypersonic flight vehicles; Trajectory tracking control.
Copyright © 2025 Elsevier Ltd. All rights reserved.
Conflict of interest statement
Declaration of competing interests The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.
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