Files
radar_data_process/data_process_class_dll/data_process.cpp
T
waiwaylee e9b8a3245a 更新:1、kalman_filter_init_2dots函数中量测噪声协方差矩阵R中R[1][0]赋值错误;
2、数据预处理中波位号判断规则修改;
3、数据预处理中增加点迹数量限制,避免超过数组上限;
4、Dot_Coh_TAS::dot_coh_tas_process中增加容器非空判断;
5、d_cal_with_doppler中计算雅可比矩阵改为用预测值计算;
6、tmp_track_to_trust_track中数组索引为负的问题修复;
7、tmp_track_to_trust_track中对容器push_back后在修改元素可能导致无法修改容器中的元素;
8、修改部分参数,适配机扫模式;

Signed-off-by: waiwaylee <waiwaylee@foxmail.com>
2026-07-06 14:21:49 +08:00

278 lines
7.2 KiB
C++

#include "data_process.h"
#include "memory.h"
#include <QVector>
#include <qmath.h>
#include <iostream>
using namespace std;
/*******************************************************************************/
/*******************************************************************************/
/************************************用户接口函数*******************************/
/*******************************************************************************/
/*******************************************************************************/
//数据预处理
int Data_Process::data_preprocess(struct DataRev Data_Input[150])
{
//数据存入缓存区域 Data_buffer
if(Data_Input[0].point_type == 0) //tws数据
{
data_num=min(Data_Input[0].Point_Sum, 150);
TAS_track_idx = Data_Input[0].TAS_track_index;
for (int i=0; i<data_num;i++)
{
PointRecv Data_buffer_temp;
Data_buffer_temp.Amplitude=Data_Input[i].Amplitude;
Data_buffer_temp.Azimuth=Data_Input[i].Azimuth/180*PI;
Data_buffer_temp.snr = Data_Input[i].Snr;
Data_buffer_temp.RCS = Data_Input[i].RCS;
Data_buffer_temp.CPI_Time = Data_Input[i].CPI_time;
Data_buffer_temp.Freq_index = Data_Input[i].Freq_index;
Data_buffer_temp.PRF_index = Data_Input[i].PRI;
Data_buffer_temp.Range = Data_Input[i].Range;
Data_buffer_temp.Height= Data_Input[i].Range*sin(Data_Input[i].Elevation/180*PI);
Data_buffer_temp.Use_Flag = 0;
Data_buffer_temp.Velocity = Data_Input[i].Velocity;
Data_buffer_temp.pitch_num = Data_Input[i].pitch_num;
std::memcpy(Data_buffer_temp.speed_dim, Data_Input[i].speed_dim, sizeof(Data_buffer_temp.speed_dim));
std::memcpy(Data_buffer_temp.range_dim, Data_Input[i].range_dim, sizeof(Data_buffer_temp.range_dim));
Data_buffer.push_back(Data_buffer_temp);
}
if(Data_Input[0].Beam_index_aiz % 16 == 0) //TWS
{
return 1;
}
else
{
return 2;
}
}
else if(Data_Input[0].point_type == 1) //tas数据
{
// qDebug() << "TAS TARGET :" <<Data_Input[0].TAS_track_index;
// qDebug() << "TAS POINT :" <<Data_Input[0].Point_Sum;
data_num=Data_Input[0].Point_Sum;
TAS_track_idx = Data_Input[0].TAS_track_index;
for (int i=0; i<data_num;i++)
{
PointRecv Data_buffer_temp;
Data_buffer_temp.Amplitude=Data_Input[i].Amplitude;
Data_buffer_temp.Azimuth=Data_Input[i].Azimuth/180*PI;
Data_buffer_temp.snr = Data_Input[i].Snr;
Data_buffer_temp.RCS = Data_Input[i].RCS;
Data_buffer_temp.CPI_Time = Data_Input[i].CPI_time;
Data_buffer_temp.Freq_index = Data_Input[i].Freq_index;
Data_buffer_temp.PRF_index = Data_Input[i].PRI;
Data_buffer_temp.Range = Data_Input[i].Range;
Data_buffer_temp.Height= Data_Input[i].Range*sin(Data_Input[i].Elevation/180*PI);
Data_buffer_temp.Use_Flag = 0;
Data_buffer_temp.Velocity = Data_Input[i].Velocity;
Data_buffer_temp.pitch_num = Data_Input[i].pitch_num;
std::memcpy(Data_buffer_temp.speed_dim, Data_Input[i].speed_dim, sizeof(Data_buffer_temp.speed_dim));
std::memcpy(Data_buffer_temp.range_dim, Data_Input[i].range_dim, sizeof(Data_buffer_temp.range_dim));
Data_buffer_tas.push_back(Data_buffer_temp);
// qDebug() << "Azimuth:" << Data_Input[i].Azimuth
// << "Range:" << Data_Input[i].Range
// << "EL:" << Data_Input[i].Elevation
// << "CPI_Time"<< Data_Input[i].CPI_time
// << "data_num:" << data_num;
}
return 3;
}
else
{
return 0;
}
}
//数据处理
int Data_Process::track_process(struct Track Trust_Track_Output[MAX_TRACK_NUM][10],
int *Trust_track_num_Output,
int Track_die_Index_Output[],
int *Track_die_num_Output,
int model)
{
//TWS处理
if(model==2)
{
dot_coh.dot_coh_process_buff(&Data_buffer,&point_recv,Work_Parameter);
QVector<PointRecv>().swap(Data_buffer);
}
if(model==1)
{
*Trust_track_num_Output=0; //航迹更新数
*Track_die_num_Output=0; //航迹消亡数目
track_asso.track_asso_process(&point_recv,
&trust_track,
Trust_Track_Output,
Trust_track_num_Output,
Work_Parameter
);
track_die.track_die_process( &trust_track,
Track_die_Index_Output,
Track_die_num_Output);
track_init.track_init_process_logic( &point_recv,
&trust_track,
&temp_track,
Trust_Track_Output,
Trust_track_num_Output,
Work_Parameter);
}
// TAS处理
if(model==3)
{
*Trust_track_num_Output=0; //航迹更新数
*Track_die_num_Output=0; //航迹消亡数目
dot_coh_tas.dot_coh_tas_process(&Data_buffer_tas,&point_recv_tas); //点迹凝聚
// if(point_recv_tas.size()>0)
// {
// qDebug() << "point_recv_tas :" <<point_recv_tas[0].Azimuth/PI*180<<" "<<point_recv_tas[0].Range;
// }
QVector<PointRecv>().swap(Data_buffer_tas);//凝聚完毕 清除Data_buffer
track_asso_tas.track_asso_process_tas(&point_recv_tas, //点迹文件
&trust_track, //航迹文件
Trust_Track_Output, //更新航迹信息
Trust_track_num_Output, //更新航迹数
Work_Parameter, //工作参数
TAS_track_idx);
QVector<PointRecv>().swap(point_recv_tas); //清除 point_recv_tas
track_die_tas.track_die_process_tas( &trust_track,
Track_die_Index_Output,
Track_die_num_Output);
}
return 1;
}
//波束控制
void Data_Process::Beam_Ctrl(struct TrackingBeam *Tracking_beam,
struct Track Trust_Track_Output[][10],
int *Trust_track_num_Output)
{
tas_ctrl.tas_ctrl_process(&trust_track,Tracking_beam, Trust_Track_Output, Trust_track_num_Output,Work_Parameter);
}
//数据处理参数初始化
int Data_Process::track_process_parameters_initial(struct RadarPara Radar_Parameter)
{
//工作参数设置
memcpy(&Work_Parameter, &Radar_Parameter, sizeof(RadarPara));
return 0;
}
//数据处理参数修改
int Data_Process::track_process_parameters_modify(struct RadarPara Radar_Parameter)
{
memcpy(&Work_Parameter, &Radar_Parameter, sizeof(RadarPara));
return 0;
}
//航迹清空函数
int Data_Process::track_clear_all(void)
{
//清空可靠航迹
return 0;
}
//手动航迹删除函数
int Data_Process:: track_delete(int delete_track_num, //手动删除的航迹数目
int delete_track_index[]) //手动删除的航迹号
{
for (int i=0;i<delete_track_num ;i++)
{
for (int j=0;j<trust_track.size();j++)
{
if(trust_track[j].Track_Index == delete_track_index[i])
{
trust_track[j].manual_delete_flag=1;
}
}
}
return 0;
}
//手动转TAS跟踪函数
int Data_Process:: tracking_start(int track_index) //需要手动转入TAS跟踪的航迹号
{
for ( int i=0; i<trust_track.size();i++)
if(trust_track[i].Track_Index==track_index)
{
trust_track[i].manual_tracking_flag = 1;
}
return 0;
}
//手动打跟踪波束
int Data_Process::tracking_point(float Azimuth)//方位角
{
return 0;
}