舰船甲板运动状态预测及无人直升机着舰时刻优化OA
Prediction of ship deck motion state and landing time optimization of unmanned helicopters
[目的]在恶劣海况下,受风浪等因素影响,舰船甲板处于持续运动状态,无人直升机在此条件下难以实现稳定自主着舰,通常需依赖操作人员的经验进行人工遥控降落.这种降落方式不仅耗时较长,且存在较大安全隐患.因此,亟须预测舰船甲板的横摇、纵摇、沉浮幅值及其运动变化速率,确定无人直升机可安全平稳着舰的最优降落时刻,从而有效降低降落风险.[方法]为实现无人直升机最优降落时刻的预测,本文基于时间序列预测算法,采用自回归模型对舰船甲板的运动状态进行建模与预测.在此基础上,为满足无人直升机降落过程中的安全性要求,构建多目标优化数学模型,并利用模拟退火算法推算最优降落时刻,为无人直升机自主着舰提供决策依据.同时,设计并搭建了可模拟舰船甲板横摇、纵摇及沉浮运动的甲板运动模拟器,构建了自适应起落架系统以模拟无人直升机着舰过程,并对优化结果进行了验证.[结果]实验结果表明,预测数据曲线与实测数据曲线高度吻合,横摇、纵摇预测值与实测值的最大误差均小于0.01°,沉浮预测值与实测值的最大误差小于6 mm,最大相对误差均小于1%,满足工程预测精度要求.基于模拟退火算法的优化结果显示,91.50 s、96.75 s、99.25 s为舰船甲板横摇、纵摇、沉浮幅值及其变化速率均较小的关键时刻,其中91.50 s时刻的甲板综合倾斜角度与变化速率最低,表明无人直升机可在该时刻实现平稳着舰.[结论]基于自回归模型的甲板运动状态预测算法具有预测精度高、响应速度快的特点,可高效输出准确的甲板运动数据.与传统单一预测方法相比,本文通过模拟退火算法对预测结果进行多目标优化,筛选出的最优降落时刻更好地满足了无人直升机安全平稳着舰的需求.本研究成果不仅提升了无人直升机在舰船甲板复杂运动状态下的安全着舰能力,也为其他类型飞行器的舰载起降提供了参考.
[Objective]In harsh sea conditions,due to the influence of wind,waves,and other factors,the ship deck is in constant motion.In such conditions,a stable and independent landing is difficult to achieve for unmanned helicopters.Generally,the operator's experience should be relied on to achieve remote control landing.This landing method is time-consuming and has great safety hazards.Therefore,it is urgent to predict the amplitude of the roll,pitch,and ascending and descending,and the motion change rate of the ship deck for determining the optimal landing time when the unmanned helicopter can land the ship safely and stably,thus reducing landing risks.[Methods]The autoregression model was employed to model and predict the motion state of the ship deck based on the time series prediction algorithm,thus predicting the optimal landing time of the unmanned helicopter.On this basis,a multi-objective optimization mathematical model was built to meet the safety requirements during the landing of the unmanned helicopter,with the simulated annealing optimization algorithm adopted to calculate the optimal landing to provide a decision-making basis for the independent landing of unmanned helicopters.Meanwhile,a ship deck motion simulator was developed to simulate the roll,pitch,ascending and descending motion of the ship deck,with an adaptive gear system built to simulate the landing process and verify the optimization results.[Results]The experimental results indicate that the predicted data curve is highly consistent with the measured data curve.The maximum error between the predicted roll and pitch values and the measured values is less than 0.01°,and the maximum error between the predicted ascending and descending values and the measured values is less than 6 mm.The maximum relative error is less than 1%,which meets the requirements for prediction accuracy.The optimization results based on the simulated annealing algorithm show that 91.50 s,96.75 s,and 99.25 s are the key moments when the roll,pitch,ascending and descending amplitudes of the ship deck and their motion change rates are small.Specifically,the comprehensive tilt angle of the deck is the lowest,and the motion change rate is the smallest at 91.50 s,which is the time for the unmanned helicopter to stably land.[Conclusions]The prediction algorithm for deck motion state based on the autoregression model features high prediction accuracy and fast response speed.Additionally,it can efficiently calculate accurate deck motion data.Compared with the traditional prediction methods,multi-objective optimization was conducted on prediction results by adopting the simulated annealing algorithm,and the selected optimal landing time can better meet the requirements for safe and stable landing of the unmanned helicopter.This study not only improves the safe landing ability of unmanned helicopters under complex motion states of ship decks,but also provides references for the take-off and landing of other types of aircraft.
金映丽;李季濠;闫明
沈阳工业大学辽宁省冲击防护与损伤评估技术工程研究中心,辽宁沈阳 110870沈阳工业大学辽宁省冲击防护与损伤评估技术工程研究中心,辽宁沈阳 110870沈阳工业大学辽宁省冲击防护与损伤评估技术工程研究中心,辽宁沈阳 110870
信息技术与安全科学
无人直升机舰船甲板时间序列自回归模型运动状态预测模拟退火算法
unmanned helicoptershipdecktime seriesautoregression modelmotion state predictionsimulated annealing algorithm
《沈阳工业大学学报》 2026 (3)
86-92,7
国防科技创新特区项目(20-163-00-TS-006-002-01).
评论