CN113393032B - Track cycle prediction method based on resampling - Google Patents
Track cycle prediction method based on resampling Download PDFInfo
- Publication number
- CN113393032B CN113393032B CN202110658739.1A CN202110658739A CN113393032B CN 113393032 B CN113393032 B CN 113393032B CN 202110658739 A CN202110658739 A CN 202110658739A CN 113393032 B CN113393032 B CN 113393032B
- Authority
- CN
- China
- Prior art keywords
- data
- track
- batch
- resampled
- network
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000000034 method Methods 0.000 title claims abstract description 43
- 238000012952 Resampling Methods 0.000 title claims abstract description 29
- 238000012549 training Methods 0.000 claims abstract description 12
- 238000001914 filtration Methods 0.000 claims abstract description 11
- 230000004913 activation Effects 0.000 claims abstract description 10
- 238000004364 calculation method Methods 0.000 claims abstract description 4
- 238000012360 testing method Methods 0.000 claims description 19
- 238000004422 calculation algorithm Methods 0.000 claims description 18
- 238000013528 artificial neural network Methods 0.000 claims description 13
- 238000009499 grossing Methods 0.000 claims description 10
- 239000011159 matrix material Substances 0.000 claims description 10
- 238000005070 sampling Methods 0.000 claims description 10
- 230000008569 process Effects 0.000 claims description 7
- 230000006870 function Effects 0.000 claims description 6
- 238000011478 gradient descent method Methods 0.000 claims description 4
- 230000011218 segmentation Effects 0.000 claims description 4
- 238000005259 measurement Methods 0.000 claims description 3
- 230000007704 transition Effects 0.000 claims description 3
- ORILYTVJVMAKLC-UHFFFAOYSA-N Adamantane Natural products C1C(C2)CC3CC1CC2C3 ORILYTVJVMAKLC-UHFFFAOYSA-N 0.000 claims description 2
- 230000003044 adaptive effect Effects 0.000 claims description 2
- 230000002457 bidirectional effect Effects 0.000 claims description 2
- 125000004122 cyclic group Chemical group 0.000 claims description 2
- 238000005457 optimization Methods 0.000 claims description 2
- 230000006403 short-term memory Effects 0.000 claims description 2
- 230000026676 system process Effects 0.000 claims 1
- 230000033001 locomotion Effects 0.000 abstract description 11
- 238000003062 neural network model Methods 0.000 abstract description 9
- 230000008859 change Effects 0.000 abstract description 2
- 238000010606 normalization Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 5
- 238000004088 simulation Methods 0.000 description 5
- 238000007418 data mining Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000002452 interceptive effect Effects 0.000 description 2
- 238000010801 machine learning Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 238000013277 forecasting method Methods 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q10/00—Administration; Management
- G06Q10/04—Forecasting or optimisation specially adapted for administrative or management purposes, e.g. linear programming or "cutting stock problem"
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F18/00—Pattern recognition
- G06F18/20—Analysing
- G06F18/21—Design or setup of recognition systems or techniques; Extraction of features in feature space; Blind source separation
- G06F18/214—Generating training patterns; Bootstrap methods, e.g. bagging or boosting
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06N—COMPUTING ARRANGEMENTS BASED ON SPECIFIC COMPUTATIONAL MODELS
- G06N3/00—Computing arrangements based on biological models
- G06N3/02—Neural networks
- G06N3/04—Architecture, e.g. interconnection topology
- G06N3/044—Recurrent networks, e.g. Hopfield networks
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06N—COMPUTING ARRANGEMENTS BASED ON SPECIFIC COMPUTATIONAL MODELS
- G06N3/00—Computing arrangements based on biological models
- G06N3/02—Neural networks
- G06N3/08—Learning methods
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Physics & Mathematics (AREA)
- Data Mining & Analysis (AREA)
- General Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Business, Economics & Management (AREA)
- Evolutionary Computation (AREA)
- Artificial Intelligence (AREA)
- Biophysics (AREA)
- General Health & Medical Sciences (AREA)
- Human Resources & Organizations (AREA)
- Software Systems (AREA)
- Mathematical Physics (AREA)
- Economics (AREA)
- Health & Medical Sciences (AREA)
- Computing Systems (AREA)
- Molecular Biology (AREA)
- Biomedical Technology (AREA)
- Strategic Management (AREA)
- Computational Linguistics (AREA)
- Quality & Reliability (AREA)
- General Business, Economics & Management (AREA)
- Development Economics (AREA)
- Operations Research (AREA)
- Tourism & Hospitality (AREA)
- Entrepreneurship & Innovation (AREA)
- Game Theory and Decision Science (AREA)
- Marketing (AREA)
- Bioinformatics & Cheminformatics (AREA)
- Bioinformatics & Computational Biology (AREA)
- Computer Vision & Pattern Recognition (AREA)
- Evolutionary Biology (AREA)
- Radar Systems Or Details Thereof (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
Description
技术领域Technical field
本发明属于通信技术领域,特别涉及一种航迹的循环预测方法,可用于目标跟踪。The invention belongs to the field of communication technology, and particularly relates to a cycle prediction method of track, which can be used for target tracking.
背景技术Background technique
目标轨迹预测技术是对目标未来的轨迹状态信息进行准确预测,是目标跟踪领域的关键技术之一。Target trajectory prediction technology is to accurately predict the target's future trajectory status information and is one of the key technologies in the field of target tracking.
随着航空飞行环境趋向复杂化,由于系统误差、气象恶劣、传感器本身的性能异常等不确定因素的影响,将会造成传感器无法继续探测到目标航迹信息,影响飞行安全的问题。因此需要具备一定的航迹预测的能力,为后续目标跟踪提供更完整的数据信息,确保飞行安全。As the aviation flight environment becomes more complex, due to the influence of uncertain factors such as system errors, bad weather, and abnormal performance of the sensor itself, the sensor will be unable to continue to detect target track information, affecting flight safety. Therefore, it is necessary to have certain trajectory prediction capabilities to provide more complete data information for subsequent target tracking and ensure flight safety.
目前,航迹预测算法主要分为基于飞行性能参数的动力学模型、基于参数最优估计模型以及基于历史数据的机器学习方法。At present, trajectory prediction algorithms are mainly divided into dynamic models based on flight performance parameters, parameter optimal estimation models and machine learning methods based on historical data.
在动力学模型方面,付强在论文航迹预测方法在航路飞行中的应用剖析中提出了基于大圆航线和等角航线的航迹预测方法,在模型中引入了圆航线和等角航线等信息。廖超伟在论文航空器跑道滑行轨迹预测方法中提出了一种基于空气动力学的轨迹预测方法,该方法对目标进行受力分析,建立滑行动力学模型。Porretta在论文PerformanceEvaluation of a Novel 4D Trajectory Prediction Model for Civil Aircraft中提出了一种综合考虑风速、飞机的横向制动力和速度估计的飞机性能模型。但这些方法所需要的模型参数比如气象预报、场面管制意图、飞行计划信息等在实际运用中较难获取到,因而在这些模型参数缺失的情况下,无法准确对目标进行建模,会导致预测结果不准确。In terms of dynamic models, Fu Qiang proposed a trajectory prediction method based on great circle routes and equiangular routes in his paper Analysis of the Application of Track Prediction Methods in Route Flights, and introduced information such as circular routes and equiangular routes into the model. . In his paper, aircraft runway taxiing trajectory prediction method, Liao Chaowei proposed a trajectory prediction method based on aerodynamics. This method analyzes the force of the target and establishes a taxiing dynamics model. In the paper PerformanceEvaluation of a Novel 4D Trajectory Prediction Model for Civil Aircraft, Porretta proposed an aircraft performance model that comprehensively considers wind speed, the aircraft's lateral braking force and speed estimation. However, the model parameters required by these methods, such as weather forecasts, surface control intentions, flight plan information, etc., are difficult to obtain in actual applications. Therefore, in the absence of these model parameters, the target cannot be accurately modeled, which will lead to prediction The results are inaccurate.
在参数最优估计方面,最经典的算法是基于卡尔曼滤波进行目标状态估计,来预测航空器的轨迹。宫淑丽在论文基于IMM算法的机场场面运动目标跟踪中提出了基于交互式多模型结合无迹卡尔曼滤波算法,此算法对飞机的运动过程进行建模,并进行轨迹的预测计算。汤新民在论文基于混杂系统理论的无冲突4D航迹预测中提出了基于混杂系统理论的航迹预测算法,此算法针对航空器在不同航段内的运动特点,构建了航空器动力学模型的参数演化模型,并且构建了状态转移模型对不同航段之间的切换进行建模,通过调整相应的参数完成航空器的航迹预测。但此类算法执行效率较低,且在不知道目标运动状态时,无法准确对目标进行建模,进而导致预测航迹误差较大。在机器学习模型方面,马勇在论文基于数据挖掘的四维航迹精密预测方法研究中提出了一种基于数据挖掘的精密航迹预测方法,该方法首先对历史航迹进行聚类,然后求出每个聚类的密集轨迹,并结合隐马尔科夫模型实现航空运输网络的地图匹配,以完成精确的航迹预测。此类算法比经典预测方法预测更为准确,但是仍存在预测时长较短的问题。In terms of parameter optimal estimation, the most classic algorithm is to estimate the target state based on Kalman filter to predict the trajectory of the aircraft. In her paper on tracking moving targets on airport surfaces based on the IMM algorithm, Gong Shuli proposed an algorithm based on interactive multi-model combined with unscented Kalman filtering. This algorithm models the movement process of the aircraft and performs trajectory prediction calculations. Tang Xinmin proposed a trajectory prediction algorithm based on hybrid system theory in his paper Conflict-free 4D trajectory prediction based on hybrid system theory. This algorithm constructs the parameter evolution of the aircraft dynamics model based on the movement characteristics of the aircraft in different flight segments. model, and built a state transition model to model the switching between different flight segments, and completed the aircraft trajectory prediction by adjusting the corresponding parameters. However, this type of algorithm has low execution efficiency, and cannot accurately model the target when the target's motion state is unknown, resulting in large errors in predicted track. In terms of machine learning models, Ma Yong proposed a precise track prediction method based on data mining in his paper Research on the Precision Prediction Method of Four-Dimensional Tracks Based on Data Mining. This method first clusters historical tracks and then calculates The dense trajectories of each cluster are combined with the hidden Markov model to achieve map matching of the air transportation network to complete accurate trajectory prediction. This type of algorithm is more accurate in forecasting than classic forecasting methods, but still suffers from the problem of shorter forecasting time.
综上,现有目标航迹预测技术均存在误差大、预测模型单一,预测时长较短的不足,导致预测航迹准确性差,影响飞行安全。In summary, existing target trajectory prediction technologies have the disadvantages of large errors, single prediction models, and short prediction duration, resulting in poor accuracy of predicted trajectory and affecting flight safety.
发明内容Contents of the invention
本发明的目的在于针对上述现有技术的不足,提出一种基于重采样下的循环预测方法,以减少机动目标航迹的预测误差,增加预测时长,提高航迹预测准确性。The purpose of the present invention is to propose a cyclic prediction method based on resampling to reduce the prediction error of maneuvering target tracks, increase the prediction time, and improve the accuracy of track prediction in view of the above-mentioned shortcomings of the existing technology.
本发明的技术方案是,对目标历史航迹数据进行预处理;构建并训练神经网络模型;运用循环策略生成部分历史航迹数据,并利用训练好的网络模型参数对其进行计算;对计算结果进行平滑滤波,得到最终预测航迹。The technical solution of the present invention is to preprocess the target historical track data; construct and train a neural network model; use a loop strategy to generate part of the historical track data, and use the trained network model parameters to calculate it; and calculate the calculation results Perform smoothing filtering to obtain the final predicted track.
根据上述思路,本发明基于重采样下的航迹循环预测方法,其特征在于,包括如下:According to the above ideas, the present invention is based on the track cycle prediction method under resampling, which is characterized by including the following:
(1)对机动目标的历史航迹数据进行滤波和归一化处理;(1) Filter and normalize the historical track data of maneuvering targets;
(2)将重采样周期T'设为系统采样周期T的10倍,将归一化后的航迹数据采样成10根重采样航迹,作为网络数据集,并确定其输入样本维度及标签样本维度;(2) Set the resampling period T' to 10 times the system sampling period T, sample the normalized track data into 10 resampled tracks as a network data set, and determine the input sample dimensions and labels sample dimensions;
(3)构建一个依次由双向长短时记忆单元Bi-LSTM层、Dropout层、Dense层、激活层,这四层结构组成的神经网络;(3) Construct a neural network consisting of four layers of bidirectional long short-term memory unit Bi-LSTM layer, Dropout layer, Dense layer, and activation layer;
(4)设置最大迭代次数为N和批量大小batch_size,将网络数据集送入搭建好的网络中,运用批量梯度下降法对其网络的参数进行迭代训练,当迭代次数到达N时,得到训练好的网络模型;(4) Set the maximum number of iterations to N and the batch size batch_size, send the network data set to the built network, and use the batch gradient descent method to iteratively train the parameters of the network. When the number of iterations reaches N, the training is completed network model;
(5)对未来一段时间的航迹进行预测:(5) Predict the trajectory in the future:
(5a)采用循环策略处理重采样后的10根航迹数据,以生成用于预测未来航迹的10批数据;(5a) Use a loop strategy to process the 10 resampled track data to generate 10 batches of data for predicting future tracks;
(5b)对循环策略处理后的10批数据通过调用训练好的神经网络参数对其依次进行计算,得到10根预测航迹,并将10根航迹按照重采样前的原始时隙的顺序组合成一根预测航迹;(5b) Calculate the 10 batches of data processed by the loop strategy sequentially by calling the trained neural network parameters to obtain 10 predicted tracks, and combine the 10 tracks in the order of the original time slots before resampling Predict the trajectory into one root;
(6)对预测航迹采用smooth方法进行平滑滤波处理,获得最终预测结果。(6) Use the smooth method to perform smoothing filtering on the predicted trajectory to obtain the final prediction result.
本发明与现有技术相比,具有以下优点:Compared with the prior art, the present invention has the following advantages:
1)本发明运用神经网络的Bi-LSTM层双向读取目标的历史航迹并学习其变化特征,当目标运动状态在未来发生改变时,仍然可以较为准确的预测出未来航迹。1) This invention uses the Bi-LSTM layer of the neural network to bidirectionally read the historical track of the target and learn its changing characteristics. When the target's motion state changes in the future, it can still predict the future track relatively accurately.
2)本发明运用重采样策略对历史航迹在不同时隙下进行重采样,可以使数据集更能均衡的体现历史航迹的变化信息,减少了神经网络预测航迹的预测误差,进一步提高预测准确性。2) The present invention uses a resampling strategy to resample the historical track in different time slots, which can make the data set more balanced to reflect the change information of the historical track, reduce the prediction error of the neural network predicted track, and further improve Forecast accuracy.
3)本发明对重采样后的航迹数据采用循环策略生成多批数据,并对多批数据依次进行预测,相比于传统的单次预测方法更大限度的利用了已知航迹的数据信息,可以获得预测时长较长的预测航迹,为目标提供更为准确的飞行策略,确保目标飞行安全。3) The present invention uses a loop strategy to generate multiple batches of data for the resampled track data, and predicts the multiple batches of data in sequence. Compared with the traditional single prediction method, the present invention makes greater use of the data of the known track. Information can be used to obtain a predicted trajectory with a longer prediction time, provide a more accurate flight strategy for the target, and ensure the safety of the target flight.
附图说明Description of drawings
图1为本发明的实现流程图;Figure 1 is a flow chart of the implementation of the present invention;
图2为本发明使用的神经网络模型结构图。Figure 2 is a structural diagram of the neural network model used in the present invention.
具体实施方式Detailed ways
下面结合附图对本发明的实施例和效果作进一步详细描述。The embodiments and effects of the present invention will be described in further detail below with reference to the accompanying drawings.
参照图1,本发明基于重采样下的航迹循环预测方法,实现步骤如下:Referring to Figure 1, the present invention is based on the track cycle prediction method under resampling. The implementation steps are as follows:
步骤1,生成航迹数据集。Step 1: Generate track data set.
设置系统持续时间为3000s,系统采样周期T为1s,过程演化噪声方差0.01,目标x轴初始速度200m/s,y轴初始速度200m/s,z轴初始速度0m/s,x轴起始坐标为15,y轴起始坐标15,z轴起始坐标15000m;Set the system duration to 3000s, the system sampling period T to 1s, the process evolution noise variance to 0.01, the target x-axis initial speed to 200m/s, the y-axis initial speed to 200m/s, the z-axis initial speed to 0m/s, and the x-axis starting coordinate is 15, the starting coordinate of the y-axis is 15, and the starting coordinate of the z-axis is 15000m;
目标做以600s为一周期的周期性运动,单周期内的机动状态参数,如1表所示:The target performs periodic motion with a cycle of 600s. The maneuvering state parameters within a single cycle are as shown in Table 1:
表1部分时段目标机动信息Table 1 Target maneuver information in some periods
表1为目标在第一周期内(0~600s)的机动状态变化,单周期内持续300s的匀速运动,150s的左转弯运动,150s的右转弯运动。目标整个轨迹共五个周期,持续3000s。并设目标航迹的前2400s为已知的历史航迹,后600s为未知的未来航迹。Table 1 shows the target's maneuvering state changes in the first period (0 to 600s). In a single period, it lasts for 300s of constant speed movement, 150s of left turning movement, and 150s of right turning movement. The entire trajectory of the target has a total of five cycles, lasting 3000s. It is also assumed that the first 2400s of the target track are the known historical track, and the last 600s are the unknown future track.
通过雷达传感器观测平台对目标进行观测,观测采样频率设为1s,雷达延迟设为1s,基于雷达角度和半径加入观测噪声,噪声大小设为[0.001°,100m];The target is observed through the radar sensor observation platform, the observation sampling frequency is set to 1s, the radar delay is set to 1s, observation noise is added based on the radar angle and radius, and the noise size is set to [0.001°, 100m];
使用交互式多模型算法对以上目标的运动状态进行拟合,生成目标的前2400s的已知航迹数据和后600s的未知航迹数据。An interactive multi-model algorithm is used to fit the motion state of the above target, and the known track data of the first 2400s and the unknown track data of the last 600s are generated.
步骤2,对目标前2400s已知航迹信息进行卡尔曼滤波处理。Step 2: Perform Kalman filtering on the known track information of the target 2400s before.
(2.1)计算目标下一时刻k的状态预测值和误差协方差Pk|k-1:(2.1) Calculate the state prediction value of the target at the next moment k and error covariance P k|k-1 :
其中,k为离散时间周期,F为目标状态转移矩阵,T为矩阵转置,为当前时刻状态值,Pk-1|k-1为当前时刻的误差协方差,Q为过程噪声协方差矩阵;Among them, k is the discrete time period, F is the target state transition matrix, T is the matrix transpose, is the state value at the current moment, P k-1|k-1 is the error covariance at the current moment, Q is the process noise covariance matrix;
(2.2)计算航迹状态更新值和误差协方差更新值Pk|k:(2.2) Calculate track status update value and error covariance update value P k|k :
Pk|k=[I-[Pk|k-1HT(HPk|k-1HT+R)-1]H]Pk|k-1,P k|k =[I-[P k|k-1 H T (HP k|k-1 H T +R) -1 ]H]P k|k-1 ,
其中,H为航迹的观测矩阵,R为量测噪声协方差矩阵,Zk为k时刻雷达量测数据,I为单位阵;Among them, H is the observation matrix of the track, R is the measurement noise covariance matrix, Z k is the radar measurement data at time k, and I is the unit matrix;
(2.3)重复(2.1)和(2.2)共2400次,获得滤波后的航迹。(2.3) Repeat (2.1) and (2.2) a total of 2400 times to obtain the filtered trajectory.
步骤3,对滤波后的航迹进行归一化处理,得到归一化后的航迹数据Xs:Step 3: Normalize the filtered track to obtain the normalized track data X s :
其中,xi为滤波后航迹的第i个时隙数据。Among them, xi is the i-th time slot data of the filtered track.
步骤4,将归一化后的航迹数据Xs采样成10根重采样航迹。Step 4: Sample the normalized track data X s into 10 resampled tracks.
本步骤的具体实现如下:The specific implementation of this step is as follows:
以第1根重采样航迹选取原航迹的第1个时隙作为起始点,进行重采样间隔T'为10s的重采样;Use the first resampled track to select the first time slot of the original track as the starting point, and perform resampling with a resampling interval T' of 10s;
以第2根重采样航迹选取原航迹的第2个时隙作为起始点,进行重采样间隔T'为10s的重采样;Use the second resampled track to select the second time slot of the original track as the starting point, and perform resampling with a resampling interval T' of 10s;
以此类推,第10根重采样航迹选取原航迹的第10个时隙作为起始点,进行重采样间隔T'为10s的重采样;By analogy, the 10th resampled track selects the 10th time slot of the original track as the starting point, and performs resampling with a resampling interval T' of 10s;
每根重采样航迹包含300个采样点,得到重采样的10根航迹的时隙和原始航迹的时隙对应关系,如表2:Each resampled track contains 300 sampling points, and the corresponding relationship between the time slots of the 10 resampled tracks and the time slots of the original track is obtained, as shown in Table 2:
表2重采样航迹与原航迹时隙对应表Table 2 Correspondence table between resampled tracks and original track time slots
步骤5,确定网络输入样本维度及标签样本维度。Step 5: Determine the network input sample dimensions and label sample dimensions.
本步骤的具体实现如下:The specific implementation of this step is as follows:
对于网络输入样本维度的确定:是先确定输入样本滑动窗口长度W为120,特征数目为1;之后对重采样后的10根航迹数据按照W依次进行滑动分割,并将分割结果进行拼接,获得样本的样本批量为610、维度为610*120*1的网络输入样本;To determine the dimension of the network input sample: first determine the input sample sliding window length W as 120 and the number of features as 1; then perform sliding segmentation on the resampled 10 track data in sequence according to W, and splice the segmentation results. Obtain the network input sample with a sample batch size of 610 and a dimension of 610*120*1;
对于标签样本维度的确定:设标签样本的样本批量和特征数目与输入样本相同,设每批样本的时间步数为60,即可得到维度为610*60*1的标签样本;For the determination of the label sample dimension: Assume that the sample batch and number of features of the label sample are the same as the input sample, and the time steps of each batch of samples are 60, then a label sample with a dimension of 610*60*1 can be obtained;
输入样本和标签样本所对应的重采样航迹时隙,如表3:The resampling track time slot corresponding to the input sample and label sample is as shown in Table 3:
表3输入样本/标签样本与航迹时隙对应表Table 3 Correspondence table between input samples/label samples and track time slots
步骤6,构建神经网络模型。Step 6: Build the neural network model.
参照图2,本步骤构建的神经网络模型自上而下依次由Bi-LSTM层、Dropout层、Dense层、激活层这四层结构组成,每层功能及参数如下:Referring to Figure 2, the neural network model constructed in this step consists of four layers: Bi-LSTM layer, Dropout layer, Dense layer, and activation layer from top to bottom. The functions and parameters of each layer are as follows:
Bi-LSTM层,用于提取历史航迹数据集的变化特征,其隐藏节点数units为200;The Bi-LSTM layer is used to extract the changing characteristics of the historical track data set, and its hidden node number units is 200;
Dropout层,用于防止网络在训练过程中的过拟合,其丢弃率dropout_ratio为0.2;The Dropout layer is used to prevent overfitting of the network during the training process, and its dropout rate dropout_ratio is 0.2;
Dense层,用于网络训练时拟合标签样本Y_train,其隐藏节点数units为60;The Dense layer is used to fit the label sample Y_train during network training, and its hidden node number units is 60;
激活层,用于增强网络模型对非线性数据的适应性,其激活函数为linear激活函数。The activation layer is used to enhance the adaptability of the network model to nonlinear data, and its activation function is a linear activation function.
步骤7,训练神经网络模型。Step 7, train the neural network model.
训练神经网络的现有方法有批量梯度下降法、随机梯度下降法、迷你梯度下降法,本步骤采用但不限于批量梯度下降法,其实现如下:Existing methods for training neural networks include batch gradient descent, stochastic gradient descent, and mini gradient descent. This step uses but is not limited to the batch gradient descent method, which is implemented as follows:
(7.1)设置数据批量大小batch_size为64,将航迹数据集按照数据批量大小分割成多个小批量数据,将这些小批量数据依次送入神经网络中进行单次训练;(7.1) Set the data batch size batch_size to 64, divide the track data set into multiple small batches of data according to the data batch size, and send these small batches of data to the neural network in turn for single training;
(7.2)设置网络优化算法为自适应矩估计算法Adam,通过计算和校正每轮训练梯度的一阶矩和二阶矩来优化网络参数;(7.2) Set the network optimization algorithm to the adaptive moment estimation algorithm Adam, and optimize the network parameters by calculating and correcting the first-order moment and second-order moment of each round of training gradient;
(7.3)设置网络最大迭代次数为100,重复(7.1)和(7.2)达到最大的迭代次数,得到训练好的网络模型。(7.3) Set the maximum number of iterations of the network to 100, repeat (7.1) and (7.2) to reach the maximum number of iterations, and obtain the trained network model.
步骤8,生成用于预测未来航迹的10批数据。Step 8: Generate 10 batches of data for predicting future trajectories.
本步骤的具体实现如下:The specific implementation of this step is as follows:
(8.1)根据航迹需要预测的时长Tpre、重采样周期T'和系统采样周期T,计算10批数据的预测批次N:(8.1) Calculate the prediction batch N of 10 batches of data according to the duration T pre that needs to be predicted, the resampling period T' and the system sampling period T:
N=Tpre/T/T',N=T pre /T/T',
其中,本实例中Tpre为600s,T为1s,T'为10s,由公式得到预测批次N为60;Among them, in this example, T pre is 600s, T is 1s, T' is 10s, and the predicted batch N is 60 according to the formula;
(8.2)对10根重采样航迹采用循环策略选取60批测试数据以生成10批数据:(8.2) Use a loop strategy to select 60 batches of test data for 10 resampled tracks to generate 10 batches of data:
对第1批数据的第1批次测试数据,选取第1根重采样航迹的第62~181时隙的航迹数据;For the first batch of test data of the first batch of data, select the track data of the 62nd to 181st time slots of the first resampled track;
对第1批数据的第2批次的测试数据,选取第1根重采样航迹的第63~182时隙的航迹数据;For the test data of the second batch of the first batch of data, select the track data of the 63rd to 182nd time slots of the first resampled track;
以此类推,对第1批数据的第60批次的测试数据,选取第1根重采样航迹的第121~240时隙的航迹数据;By analogy, for the test data of the 60th batch of the first batch of data, the track data of the 121st to 240th time slots of the first resampled track are selected;
对第2批数据的第1批次测试数据,选取第2根重采样航迹的第62~181时隙的航迹数据;For the first batch of test data of the second batch of data, select the track data of the 62nd to 181st time slots of the second resampled track;
对第2批数据的第2批次的测试数据,选取第2根重采样航迹的第63~182时隙的航迹数据;For the test data of the second batch of data, select the track data of the 63rd to 182nd time slots of the second resampled track;
以此类推,对第10批数的第60批次的测试数据,选取第10根重采样航迹的第121~240时隙的航迹数据。By analogy, for the test data of the 60th batch of the 10th batch, the track data of the 121st to 240th time slots of the 10th resampled track are selected.
60批测试数据与重采样后的10根航迹时隙对应关系,如表4:The corresponding relationship between 60 batches of test data and the 10 resampled track time slots is shown in Table 4:
表4网络输入重采样后航迹时隙对应表Table 4. Track time slot correspondence table after network input resampling
步骤9,对循环策略处理后的10批数据通过调用训练好的神经网络参数对其依次进行计算,得到10根预测航迹。Step 9: Calculate the 10 batches of data processed by the loop strategy sequentially by calling the trained neural network parameters to obtain 10 predicted tracks.
(9.1)对(8.2)中得到的第1批数据的60批测试数据依次进行计算:(9.1) Calculate the 60 batches of test data of the first batch of data obtained in (8.2) in sequence:
调用训练好的网络参数对第1批数据的第1批次测试数据进行计算,得到182~241时隙的航迹;Call the trained network parameters to calculate the first batch of test data of the first batch of data, and obtain the trajectory of time slots 182 to 241;
调用训练好的网络参数对第1批数据的第2批次测试数据进行计算,得到183~242时隙的航迹;Call the trained network parameters to calculate the second batch of test data of the first batch of data, and obtain the trajectory of time slots 183 to 242;
以此类推,调用训练好的网络参数对第1批数据的第60批次测试数据进行计算,得到241~300时隙的航迹,By analogy, the trained network parameters are called to calculate the 60th batch of test data of the first batch of data, and the trajectory of time slots 241 to 300 is obtained.
上述共得到的60批预测结果,其与重采样后的航迹时隙对应关系,如表5:The corresponding relationship between the 60 batches of prediction results obtained above and the resampled track time slots is shown in Table 5:
表5 60批预测结果与重采样后航迹时隙对应表Table 5 Correspondence table of 60 batches of prediction results and track time slots after resampling
(9.2)依次选取60批预测结果的最后一个时隙点,拼接成含有60个时隙点的预测航迹,即在第1预测批次中选择预测结果的最后一个时隙点241,在第2预测批次中选择预测结果的最后一个时隙点242,以此类推,在第60预测批次中选择预测结果的最后一个时隙点300,将这些数据依次拼接组成含有60个时隙点的航迹数据,即为第1批数据的预测航迹。(9.2) Select the last time slot point of 60 batches of prediction results in sequence and splice it into a predicted track containing 60 time slot points, that is, select the last time slot point 241 of the prediction result in the first prediction batch, and then select the last time slot point 241 of the prediction result in the first prediction batch. 2 Select the last time slot point 242 of the prediction result in the 2 prediction batch, and so on, select the last time slot point 300 of the prediction result in the 60th prediction batch, and splice these data in sequence to form 60 time slot points The track data is the predicted track of the first batch of data.
(9.3)采用(9.1)和(9.2)的方法对第2~9批数据进行预测,得到第2~9批数据的预测航迹,(9.3) Use the methods (9.1) and (9.2) to predict the 2nd to 9th batches of data to obtain the predicted tracks of the 2nd to 9th batches of data,
(9.4)将(9.1)-(9.3)得到的10根预测航迹按照重采样前的原始时隙顺序组合成一根预测航迹。(9.4) Combine the 10 predicted tracks obtained from (9.1)-(9.3) into one predicted track in the order of the original time slots before resampling.
步骤10,对预测航迹采用smooth方法进行平滑滤波处理,得到最终的预测结果。Step 10: Use the smooth method to perform smoothing filtering on the predicted trajectory to obtain the final prediction result.
平滑滤波的公式如下:The formula of smoothing filter is as follows:
yy(n)=(y(1)+y(2)+y(3)+...+y(n))/n,yy(n)=(y(1)+y(2)+y(3)+...+y(n))/n,
其中y(n)表示第n个元素平滑前的数值,yy(n)表示第n个元素平滑后的数值,经过平滑后的预测航迹即为最终的预测结果。Among them, y(n) represents the value of the nth element before smoothing, yy(n) represents the value of the nth element after smoothing, and the smoothed predicted trajectory is the final prediction result.
本发明的效果可通过以下仿真实验进一步说明。The effect of the present invention can be further illustrated through the following simulation experiments.
一.仿真条件:1. Simulation conditions:
神经网络模型以Python3.6的Keras框架为仿真平台;The neural network model uses the Keras framework of Python 3.6 as the simulation platform;
航迹生成部分和Kalman滤波部分以MATLAB 2018a为仿真平台;The track generation part and Kalman filtering part use MATLAB 2018a as the simulation platform;
二.仿真内容:2. Simulation content:
在上述条件下,采用本发明和现有两种航迹预测算法分别对目标未来600s航迹进行长时间预测,得到预测结果,如表6所示:Under the above conditions, the present invention and the existing two trajectory prediction algorithms are used to predict the target's trajectory for the next 600s for a long time, and the prediction results are obtained, as shown in Table 6:
表6不同航迹预测算法结果对比Table 6 Comparison of results of different trajectory prediction algorithms
从表6可以看出,本发明提出的基于重采样下的航迹循环预测方法相较于与现有算法,预测航迹时具有更低的误差,预测时长更长,可为目标提供更为准确的飞行策略,确保目标飞行安全。It can be seen from Table 6 that compared with the existing algorithm, the track cycle prediction method based on resampling proposed by the present invention has lower error when predicting the track, the prediction time is longer, and can provide more accurate targets for the target. Accurate flight strategy to ensure target flight safety.
以上描述仅是本发明的一个具体实例,并未构成对本发明的任何限制,显然对于本领域的专业人员来说,在了解本发明内容和原理后,都可能在不背离本发明原理、结构思想的情况下,进行形式和细节上的各种修改和改变,但是这些基于本发明思想的修正和改变仍在本发明的权利要求保护范围之内。The above description is only a specific example of the present invention and does not constitute any limitation on the present invention. Obviously, for professionals in the field, after understanding the content and principles of the present invention, it is possible to make decisions without departing from the principles and structural ideas of the present invention. Under the circumstances, various modifications and changes in form and details are made, but these modifications and changes based on the idea of the present invention are still within the scope of the claims of the present invention.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202110658739.1A CN113393032B (en) | 2021-06-15 | 2021-06-15 | Track cycle prediction method based on resampling |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202110658739.1A CN113393032B (en) | 2021-06-15 | 2021-06-15 | Track cycle prediction method based on resampling |
Publications (2)
Publication Number | Publication Date |
---|---|
CN113393032A CN113393032A (en) | 2021-09-14 |
CN113393032B true CN113393032B (en) | 2023-09-12 |
Family
ID=77620808
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202110658739.1A Active CN113393032B (en) | 2021-06-15 | 2021-06-15 | Track cycle prediction method based on resampling |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN113393032B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114048889B (en) * | 2021-10-08 | 2022-09-06 | 天津大学 | Aircraft trajectory prediction method based on long-term and short-term memory network |
CN114462293B (en) * | 2021-10-27 | 2023-10-13 | 中国空气动力研究与发展中心计算空气动力研究所 | Hypersonic speed target medium-long term track prediction method |
CN114692678B (en) * | 2022-03-14 | 2024-12-13 | 中国船舶重工集团公司第七一九研究所 | A bearings-only target motion analysis method and system for surface trajectory planning |
CN115169475A (en) * | 2022-07-19 | 2022-10-11 | 重庆交通大学 | A channel early warning method, device, equipment and medium |
CN114999233B (en) * | 2022-08-05 | 2022-11-01 | 中国航天科工集团八五一一研究所 | Target intention judgment method based on track association |
CN116993778B (en) * | 2023-07-25 | 2025-07-11 | 西北工业大学 | High-speed maneuvering target tracking error compensation method based on time sequence intelligent smoothing |
CN116976956A (en) * | 2023-09-22 | 2023-10-31 | 通用技术集团机床工程研究院有限公司 | CRM system business opportunity deal prediction method, device, equipment and storage medium |
CN117648873B (en) * | 2024-01-30 | 2024-06-04 | 国网天津市电力公司电力科学研究院 | Land subsidence prediction method, training method, device, equipment |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003130948A (en) * | 2001-10-25 | 2003-05-08 | Mitsubishi Electric Corp | Target tracking apparatus |
CN108254741A (en) * | 2018-01-16 | 2018-07-06 | 中国人民解放军海军航空大学 | Targetpath Forecasting Methodology based on Recognition with Recurrent Neural Network |
CN109508812A (en) * | 2018-10-09 | 2019-03-22 | 南京航空航天大学 | A kind of aircraft Trajectory Prediction method based on profound memory network |
CA3067573A1 (en) * | 2019-01-14 | 2020-07-14 | Harbin Engineering University | Target tracking systems and methods for uuv |
-
2021
- 2021-06-15 CN CN202110658739.1A patent/CN113393032B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003130948A (en) * | 2001-10-25 | 2003-05-08 | Mitsubishi Electric Corp | Target tracking apparatus |
CN108254741A (en) * | 2018-01-16 | 2018-07-06 | 中国人民解放军海军航空大学 | Targetpath Forecasting Methodology based on Recognition with Recurrent Neural Network |
CN109508812A (en) * | 2018-10-09 | 2019-03-22 | 南京航空航天大学 | A kind of aircraft Trajectory Prediction method based on profound memory network |
CA3067573A1 (en) * | 2019-01-14 | 2020-07-14 | Harbin Engineering University | Target tracking systems and methods for uuv |
Non-Patent Citations (1)
Title |
---|
Emergency-Oriented Spatiotemporal Trajectory Pattern Recognition by Intelligent Sensor Devices;Ping Zhang;IEEE;全文 * |
Also Published As
Publication number | Publication date |
---|---|
CN113393032A (en) | 2021-09-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN113393032B (en) | Track cycle prediction method based on resampling | |
Bellemare et al. | Autonomous navigation of stratospheric balloons using reinforcement learning | |
CN114048889B (en) | Aircraft trajectory prediction method based on long-term and short-term memory network | |
CN113569465B (en) | A joint estimation system and estimation method of track vector and target type based on deep learning | |
CN103679263B (en) | Forecasting Methodology is closed on based on the thunder and lightning of particle swarm support vector machine | |
CN103336863B (en) | The flight intent recognition methods of flight path observed data of flying based on radar | |
CN109146162B (en) | A kind of probability wind speed forecasting method based on integrated Recognition with Recurrent Neural Network | |
CN111310965A (en) | A method of aircraft track prediction based on LSTM network | |
CN112101684B (en) | Plug-in hybrid electric vehicle real-time energy management method and system | |
Xiao et al. | Vehicle trajectory interpolation based on ensemble transfer regression | |
CN111178628B (en) | Luggage arrival time prediction method and device | |
CN112348223A (en) | Missile flight trajectory prediction method based on deep learning | |
CN113408392B (en) | Flight path completion method based on Kalman filtering and neural network | |
CN109840639A (en) | A kind of late time forecasting methods of high speed rail train operation | |
CN107423412B (en) | A kind of method of the carrying robot Intelligent Recognition floor based on meteorological sensing time series pattern | |
CN115730637A (en) | Multi-mode vehicle trajectory prediction model training method and device and trajectory prediction method | |
CN104199022A (en) | Target modal estimation based near-space hypersonic velocity target tracking method | |
CN112113570B (en) | An Indoor Localization Method Based on Depth Transfer and Model Parameter Integration | |
CN115964923A (en) | Modeling method for forecasting 80-100km atmospheric wind speed in adjacent space based on VMD-PSO-LSTM | |
Han et al. | Short-term 4D trajectory prediction based on LSTM neural network | |
CN118799358A (en) | Intelligent maneuvering target tracking method and device based on long short-term memory and UT transformation | |
CN119239995A (en) | A satellite exploration control system and method based on deep reinforcement learning | |
CN116562416A (en) | Reservoir water level prediction method based on variable-mode and time-delay characteristic transducer model | |
Wang et al. | A high-precision method of flight arrival time estimation based on xgboost | |
CN119415877A (en) | A track prediction intelligent optimization system and method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |