Reliability-driven adaptive multi-level pre-optimization control method for reusable launch vehicles under strong stochastic wind disturbances

IF 13.7 1区 工程技术 Q1 ENGINEERING, INDUSTRIAL
Reliability Engineering & System Safety Pub Date : 2026-09-01 Epub Date: 2026-01-30 DOI:10.1016/j.ress.2026.112327
Dawen Huang
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引用次数: 0

Abstract

Strong stochastic wind disturbances pose a major threat to the landing reliability of reusable launch vehicles, potentially leading to attitude instability, trajectory deviation, and even structural damage. Traditional control methods, which heavily rely on precise dynamic models and online state observation or prediction, often struggle to ensure reliability under such conditions. To address this challenge, this work proposes a reliability-driven landing pre-optimization method that incorporates regional stochastic wind characteristics, thereby eliminating the need for online observation or prediction. The landing dynamics and stochastic wind field models are established to quantify the destructive impact of winds on landing reliability. An adaptive multi-level control strategy is then introduced, which hierarchically deploys simplified control laws based on real-time altitude and velocity. This design effectively compensates for time-varying wind disturbances without depending on online observers or pre-planned trajectories. Furthermore, a reliability-driven offline optimization framework is developed to tune the control parameters and landing initiation conditions. These key parameters are optimized offline through large-scale Monte Carlo simulations across diverse wind scenarios, thus avoiding the computational burden of online optimization. Finally, the optimal parameters and conditions are pre-optimized to adapt to regional stochastic winds. Results demonstrate that the proposed method achieves a landing reliability of >99.5% and reduces the maximum landing deviation by 99.52%. In comparative studies, the offline pre-optimization method shows superior performance to typical online Model Predictive Control, improving reliability by 14.1%. The proposed strategy offers a robust and practical solution for achieving high-reliability landings under strong stochastic winds.
强随机风扰动下可重复使用运载火箭可靠性驱动自适应多级预优化控制方法
强随机风扰动对可重复使用运载火箭的着陆可靠性构成重大威胁,可能导致姿态不稳定、轨迹偏离甚至结构损坏。传统的控制方法严重依赖于精确的动态模型和在线状态观测或预测,往往难以保证这种情况下的可靠性。为了应对这一挑战,本研究提出了一种可靠性驱动的着陆预优化方法,该方法结合了区域随机风特征,从而消除了在线观测或预测的需要。为了量化风对着陆可靠性的破坏性影响,建立了着陆动力学和随机风场模型。然后引入了一种自适应多级控制策略,该策略基于实时高度和速度分层部署简化的控制律。这种设计有效地补偿了时变的风干扰,而不依赖于在线观测者或预先规划的轨迹。在此基础上,建立了可靠性驱动的离线优化框架,对控制参数和起降条件进行了优化。这些关键参数通过大规模蒙特卡罗模拟在不同的风场景下进行离线优化,从而避免了在线优化的计算负担。最后,对最优参数和条件进行了预优化,以适应区域随机风。结果表明,该方法的着陆可靠性为99.5%,最大着陆偏差降低了99.52%。在对比研究中,离线预优化方法的性能优于典型的在线模型预测控制,可靠性提高14.1%。所提出的策略为在强随机风条件下实现高可靠性着陆提供了一种鲁棒性和实用性的解决方案。
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来源期刊
Reliability Engineering & System Safety
Reliability Engineering & System Safety 管理科学-工程:工业
CiteScore
15.20
自引率
39.50%
发文量
621
审稿时长
67 days
期刊介绍: Elsevier publishes Reliability Engineering & System Safety in association with the European Safety and Reliability Association and the Safety Engineering and Risk Analysis Division. The international journal is devoted to developing and applying methods to enhance the safety and reliability of complex technological systems, like nuclear power plants, chemical plants, hazardous waste facilities, space systems, offshore and maritime systems, transportation systems, constructed infrastructure, and manufacturing plants. The journal normally publishes only articles that involve the analysis of substantive problems related to the reliability of complex systems or present techniques and/or theoretical results that have a discernable relationship to the solution of such problems. An important aim is to balance academic material and practical applications.
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