杨弓熠, 周海涛, 杨春, 白涛, 姜荃. 水下航行器安全低噪发射武器优化控制研究[J]. 中国舰船研究. DOI: 10.19693/j.issn.1673-3185.03785
引用本文: 杨弓熠, 周海涛, 杨春, 白涛, 姜荃. 水下航行器安全低噪发射武器优化控制研究[J]. 中国舰船研究. DOI: 10.19693/j.issn.1673-3185.03785
Research on Optimal Control of Safety for Weapons and Low Noise during Launching for Underwater Vehicles[J]. Chinese Journal of Ship Research. DOI: 10.19693/j.issn.1673-3185.03785
Citation: Research on Optimal Control of Safety for Weapons and Low Noise during Launching for Underwater Vehicles[J]. Chinese Journal of Ship Research. DOI: 10.19693/j.issn.1673-3185.03785

水下航行器安全低噪发射武器优化控制研究

Research on Optimal Control of Safety for Weapons and Low Noise during Launching for Underwater Vehicles

  • 摘要: 【目的】水下航行器低速发射武器可大幅降低辐射噪声,但发射速度过低,可能会导致武器出管后与行进的航行器碰撞,本文构建了考虑航行器姿态、航速及侧向洋流环境等相关参数影响下的武器安全发射速度优化模型,可根据当前航行器及环境参数即时决策安全发射速度实现武器低噪声发射优化控制。【方法】首次提出一种基于危险点位移包络线的武器发射安全性评估分析方法,并基于175组工况样本采用三种数据拟合方法构建武器安全发射速度优化模型。【结果】获得多影响因素、多约束判据条件下的武器安全发射速度边界谱及武器安全发射速度优化模型,覆盖航行器俯仰角-5°至5°,航速0~4m/s及侧向洋流速度0~2m/s工况。多元多项式拟合、多项式响应面拟合及Kriging插值拟合三种算法中,Kriging插值拟合最适用于武器安全发射速度优化模型构建,拟合残差为0。【结论】航速只有在航行器存在一定俯仰角的条件下对武器安全发射速度具备显著影响。随着侧向洋流速度增大逐渐影响安全速度边界谱的下限值,随着航行器俯仰角增大逐渐影响安全速度边界谱的上限值。

     

    Abstract: Objectives Low-speed launching of weapons by underwater vehicles can greatly reduce the radiated noise. However, it may cause the collision of the weapon leaving the launch tube and the moving vehicle if the launching velocity is too low. In this paper, an optimization model of weapon safe launch velocity is constructed considering the influence of relevant parameters such as attitude, speed of the vehicle and lateral ocean current environment. The safe launch velocity can be decided immediately according to the current vehicle and environmental parameters to realize the optimal control of weapon low noise launch. Methods A method of weapon launch safety evaluation and analysis based on danger point displacement envelope is proposed for the first time, and three data fitting methods are used to construct the weapon launch velocity optimization model based on 175 working condition samples. Results The boundary spectrum and the optimization model of weapon safe launch velocity are obtained under the condition of multi-influence factors and multi-constraint criteria, which covering the vehicle pitch Angle -5° to 5°, speed 0 ~ 4m/s and lateral ocean current speed 0 ~ 2m/s conditions. Three algorithms of multivariate polynomial fitting, polynomial response surface fitting and Kriging interpolation fitting are used in this study. Kriging interpolation fitting is the most suitable for the construction of weapon safe launch velocity optimization model whose fitting residual is 0. Conclusions Speed of vehicle has a significant effect on the safe launch velocity of the weapon only when there is a certain pitch angle of the vehicle. The lower limit of the safe velocity boundary spectrum is gradually affected with the increase of lateral current velocity, and the upper limit of the safe velocity boundary spectrum is gradually affected with the increase of the pitch angle of the vehicle.

     

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