Archived
fix some bugs
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10 files changed
+110
-89
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@@ -32,7 +32,10 @@ Support method of orientation
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* As of October 5, 2024, Matlab project will no longer be considered.[ADIN 2024/10/5]
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## Project Update
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Update: 2024/11/03:
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Update: 2024/11/08:
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1. KNZ_GeoTrackLab: Fix some bug。
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Update: 2024/11/05:
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1. KNZ_GeoTrackLab: Fix some bug, Optimize UI logic。
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2. KNZ_GeoTrackLab: New added function of save and change
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file for View.
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@@ -32,6 +32,9 @@
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* 自 2024 年 10 月 5 日起,Matlab 项目将不再考虑。[ADIN 2024/10/5]
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## 项目更新
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更新:2024/11/08:
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1. KNZ_GeoTrackLab: 修复一些bug。
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更新:2024/11/05:
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1. KNZ_GeoTrackLab: 修复一些bug, 优化UI逻辑。
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2. KNZ_GeoTrackLab: 为View文本编辑器增添保存修改功能。
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+73
-64
@@ -391,13 +391,19 @@ class CALLBACK:
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# Brief : Plot by open ksln as pos solution.
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# Author: @KenanZhu All Right Reserved.
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# -------------------------------------------------------------------------------
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system = self.system.get(int(self.cfg_get['Options_Calc']['sat_system']))
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path = filedialog.askopenfilename(title='Open as Pos Solution',
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filetypes=[('Solution File(*.ksln)', '*.ksln'),
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('All Files', '*.*')])
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if not path: return
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if not path.find('.ksln'):
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plotstate.config(text='Error : Unsupported format !')
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return
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with open(path,'r')as f:
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while 1:
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line = f.readline()
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if not line: return
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if line.find('APPROX POSITION XYZ')>=0:
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apx = float(line[22:35])
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apy = float(line[35:48])
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@@ -416,23 +422,24 @@ class CALLBACK:
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elif line.find('<END OF HEADER')>=0:
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plotstate.config(text="Reading...")
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break
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satnum = 0
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ENU = np.empty((3,0))
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EPO = np.empty((1,0))
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NUM = np.empty((1,0))
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while 1:
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line = f.readline()
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if not line: return
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if line[0:1]=='>':
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satnum = 0
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EPO = np.hstack((EPO,[[float(line[1:6])]]))
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plotstate.config(text='Reading...%5d/%5d Mode: Single solving'
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%(int(line[1:6]), int(86400/ive)))
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elif line[0:1]==self.system.get(int(
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self.cfg_get['Options_Calc']['sat_system']
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)) and line.find('END')==-1 and line.find('Rec')==-1:
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satnum += 1
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elif line[0:1]==system:
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if not line.find('END')==-1: pass
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elif not line.find('Rec')==-1: pass
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else:
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satnum += 1
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elif line.find('Rec:')>=0:
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if line.find('insufficient')>=0:
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@@ -449,7 +456,7 @@ class CALLBACK:
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])
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ENU = np.hstack((ENU,S@ds))
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NUM = np.hstack((NUM,[[satnum]]))
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elif line.find('END')>=0:
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if line.find('END')>=0:
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# plot on the e
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# -------------------------------------------------------------------
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explot.clear()
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@@ -509,7 +516,6 @@ class CALLBACK:
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satnplot.set_title('Valid Satellite Numbers', loc='left', fontsize=8)
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satnplot.set_xlabel('Epochs')
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satnplot.grid(True, linestyle='--', alpha=0.7)
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canvas1.draw()
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f.close()
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@@ -545,20 +551,18 @@ class CALLBACK:
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filetypes=[('Solution File(*.ssln)', '*.ssln'),
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('All Files', '*.*')])
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if not path: return
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sattrack.clear()
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sattrack.coastlines(resolution='110m')
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sattrack.gridlines()
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if not path.find('.ssln')>=0:
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plotstate.config(text="Error : Unsupported format !")
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return
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with open(path,'r') as f:
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while 1:
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line = f.readline()
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if not line: return
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if line.find('APPROX POSITION BLH')>=0:
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sattrack.clear()
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apb = math.degrees( float(line[22:35]) )
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apl = math.degrees( float(line[35:48]) )
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plotstate.config(text="Plotting...")
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sattrack.scatter(
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apl,
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apb,
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@@ -576,63 +580,68 @@ class CALLBACK:
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transform=ccrs.PlateCarree()
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)
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canvas2.draw()
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elif line.find('GENERATE SOURCE')>=0:
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marker = line[22:26]
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elif line.find('TIME OF FIRST OBS')>=0:
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yea = int(line[22:26])
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mon = int(line[27:29])
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day = int(line[30:32])
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hou = int(line[33:35])
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min = int(line[36:38])
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sec = float(line[39:46])
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elif line.find('INTERVAL')>=0:
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ive = float(line[22:27])
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elif line.find('<END OF HEADER')>=0:
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sattrack.coastlines(resolution='110m')
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sattrack.gridlines(draw_labels=True, dms=True, x_inline=False, y_inline=False)
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sattrack.set_title('Ground Track of %s%02d (GPST: %04d/%02d/%02d/%02d/%02d/%7.04f)'
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%(system,satprn,yea,mon,day,hou,min,sec),
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loc='left',fontsize=14,weight='bold')
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break
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epoch = 0
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while 1:
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line =f.readline()
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if line[0:1]==blank:
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pass
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elif line[0:1]==system and line.find('END')==-1 and line.find('Rec')==-1:
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epoch = int(line[41:46])
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plotstate.config(text="Reading...%5d/%5d Mode: Sat track plot"
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% (int(line[41:46]), int(86400 / ive)))
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if int(line[1:3])==satprn and epoch%anirat==0:
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b = math.degrees( float(line[ 4:13]) )
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l = math.degrees( float(line[14:23]) )
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sattrack.scatter(
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l,
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b,
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color='b',
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s=2,
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transform=ccrs.PlateCarree()
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)
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canvas2.draw()
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text = sattrack.text(
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l,
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b,
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4*blank+system+'%02d'%satprn,
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color='k',
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fontsize=10,
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fontweight='bold',
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transform=ccrs.PlateCarree()
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)
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point = sattrack.scatter(
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l,
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b,
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color='b',
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s=10,
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transform=ccrs.PlateCarree()
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)
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canvas2.draw()
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text.remove()
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point.remove()
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else:
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pass
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elif line.find('END')>=0:
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plotstate.config(text="Done ! Track plot form: sys=%s sat=%2d interval=%2d"
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%(system, satprn, anirat))
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line = f.readline()
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if not line: break
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if line.find('END')>=0: break
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if not str(line[ 0: 1])==system: continue
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if not int(line[ 1: 3])==satprn: continue
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if not int(line[41:46])%anirat==0: continue
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plotstate.config(text="Reading...%5d/%5d Mode: Sat track plot"
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% (int(line[41:46]), int(86400 / ive)))
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# Judge twice
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if not int(line[ 1: 3])==satprn:break
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b = math.degrees( float(line[ 4:13]) )
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l = math.degrees( float(line[14:23]) )
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sattrack.scatter(
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l,
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b,
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color='b',
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s=2,
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transform=ccrs.PlateCarree()
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)
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canvas2.draw()
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text = sattrack.text(
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l,
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b,
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4*blank+system+'%02d'%satprn,
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color='k',
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fontsize=10,
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fontweight='bold',
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transform=ccrs.PlateCarree()
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)
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point = sattrack.scatter(
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l,
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b,
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color='b',
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s=10,
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transform=ccrs.PlateCarree()
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)
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canvas2.draw()
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text.remove()
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point.remove()
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plotstate.config(text="Done ! Track plot form: sys=%s sat=%2d interval=%2d"
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% (system, satprn, anirat))
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return
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def _Plot2polar(self, sattrack, plotstate, canvas2):
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T = threading.Thread(
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+3
-4
@@ -30,7 +30,7 @@ from matplotlib.backends.backend_tkagg import (
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import tkinter as tk
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import tkinter.font as tkfont
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import cartopy.crs as ccrs
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#import cartopy.feature as cfeature
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import cartopy.io.shapereader as shp
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import matplotlib as mpl
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mpl.use('TkAgg')
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import matplotlib.pyplot as plt
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@@ -63,7 +63,6 @@ def _instanceABO(hwndparemt, cfg_get_, func_):
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T = threading.Thread(target=lambda :instanceABO(hwndparemt, cfg_get_, func_))
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T.start()
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# noinspection PyUnusedLocal,PyProtectedMember
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class MAINGUI:
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def __init__(self, hwnd_, func_):
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@@ -395,9 +394,9 @@ class MAINGUI:
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self.sattrack.gridlines()
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fig.subplots_adjust(
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left=0,
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bottom=0.03,
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bottom=0.045,
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right=1,
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top=0.95
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top=0.90
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)
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for spine in ['right', 'left']:
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self.sattrack.spines[spine].set_visible(False)
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Binary file not shown.
Binary file not shown.
@@ -108,6 +108,17 @@
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#define GLO 04
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#define SBAS 05
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#define MAXTOE_GPS 7200.0
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#define MAXTOE_BDS 21600.0
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#define MAXTOE_GAL 14400.0
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#define MAXTOE_GLO 1800.0
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#define MAXTOE_SBS 360.0
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#define TIMEGAP_GPS 7200.0
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#define TIMEGAP_BDS 3600.0
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#define TIMEGAP_GAL 600.0
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#define TIMEGAP_GLO 1800.0
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#define MAXRINEX 4096 /* Max length of line of rinex file */
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#define MAXPATH 260 /* Max length of file path */
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+3
-6
@@ -1,10 +1,4 @@
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#include "brdm2pos.h"
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#define MAXTOE_GPS 7200.0
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#define MAXTOE_BDS 21600.0
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#define MAXTOE_GAL 14400.0
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#define MAXTOE_GLO 1800.0
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#define MAXTOE_SBS 360.0
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using namespace std;
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/**
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* Find the nearest obs epoch with boardcast.
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@@ -296,6 +290,7 @@ void read_n_b(FILE* fp_nav, pnav_body nav_b)
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case 0:
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nav_b[i_g].sPRN_BDS = -1;
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nav_b[i_g].sPRN_GAL = -1;
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nav_b[i_g].sPRN_GLO = -1;
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nav_b[i_g].sPRN_GPS = (int)strtonum(buff, 1, 2);
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nav_b[i_g].TOC_Y = (int)strtonum(buff, 4, 4);
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nav_b[i_g].TOC_M = (int)strtonum(buff, 9, 2);
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@@ -368,6 +363,7 @@ void read_n_b(FILE* fp_nav, pnav_body nav_b)
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case 0:
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nav_b[i_g].sPRN_GPS = -1;
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nav_b[i_g].sPRN_GAL = -1;
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nav_b[i_g].sPRN_GLO = -1;
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nav_b[i_g].sPRN_BDS = (int)strtonum(buff, 1, 2);
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nav_b[i_g].TOC_Y = (int)strtonum(buff, 4, 4);
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nav_b[i_g].TOC_M = (int)strtonum(buff, 9, 2);
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@@ -440,6 +436,7 @@ void read_n_b(FILE* fp_nav, pnav_body nav_b)
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case 0:
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nav_b[i_g].sPRN_BDS = -1;
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nav_b[i_g].sPRN_GPS = -1;
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nav_b[i_g].sPRN_GLO = -1;
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nav_b[i_g].sPRN_GAL = (int)strtonum(buff, 1, 2);
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nav_b[i_g].TOC_Y = (int)strtonum(buff, 4, 4);
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nav_b[i_g].TOC_M = (int)strtonum(buff, 9, 2);
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+11
-11
@@ -336,7 +336,7 @@ int sat_pos_cal(pobs_head obs_h, pobs_epoch obs_e, pobs_body obs_b,
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int sat_cal(pnav_body nav_b, pobs_head obs_h, FILE* solu,int satnum, int GNSS) {
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int ii, i, sPRN=0;
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double Min, min, Weeksec=0, Beginsec, STOP;
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double Min, min, Weeksec=0, Beginsec, STOP=0;
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pos_ts pos = { 0 };
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blh in_blh = { 0 };
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@@ -357,36 +357,36 @@ int sat_cal(pnav_body nav_b, pobs_head obs_h, FILE* solu,int satnum, int GNSS) {
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Weeksec =
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fabs(sPRN - nav_b[i].sPRN_GPS) > 0 ? Beginsec : Weeksec;
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sPRN = nav_b[i].sPRN_GPS;
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STOP = 3600.0;
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STOP = TIMEGAP_GPS/2;
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break;
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case BDS:if (nav_b[i].sPRN_BDS == -1) { continue; }
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Weeksec =
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fabs(sPRN - nav_b[i].sPRN_BDS) > 0 ? Beginsec : Weeksec;
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sPRN = nav_b[i].sPRN_BDS;
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STOP = 1800.0;
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STOP = TIMEGAP_BDS/2;
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break;
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case GAL:if (nav_b[i].sPRN_GAL == -1) { continue; }
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Weeksec =
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fabs(sPRN - nav_b[i].sPRN_GAL) > 0 ? Beginsec : Weeksec;
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sPRN = nav_b[i].sPRN_GAL;
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STOP = 300.0;
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STOP = TIMEGAP_GAL/2;
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break;
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case GLO:if (nav_b[i].sPRN_GLO == -1) { continue; }
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Weeksec =
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fabs(sPRN - nav_b[i].sPRN_GLO) > 0 ? Beginsec : Weeksec;
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sPRN = nav_b[i].sPRN_GLO;
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STOP = 900.0;
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STOP = TIMEGAP_GLO/2+18;
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break;
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}
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for (Weeksec; fabs(Weeksec - nav_b[i].TOE) <= STOP; Weeksec += 30.0) {
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if (Weeksec - Beginsec >= DAYSEC) break;
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else if (Weeksec - Beginsec >= DAYSEC - STOP) STOP += STOP;
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if (GNSS != GLO) pos = sat_pos(sPRN, i, Weeksec, GNSS, nav_b, obs_h, pos);
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else if (GNSS == GLO) pos = glo_pos(i, Weeksec, nav_b, obs_h, pos);
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for (Weeksec; fabs(Weeksec-nav_b[i].TOE)<=3600.0; Weeksec += 30.0) {
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if (Weeksec - Beginsec == 86400.0) {
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break;
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}
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pos = sat_pos(sPRN, i, Weeksec, GNSS, nav_b, obs_h, pos);
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in_blh = xyz2blh(in_blh, pos.X, pos.Y, pos.Z);
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outdata(in_blh, solu, sPRN, GNSS);
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fprintf(solu, ">>%05d", (int)(Weeksec-Beginsec)/30+1);
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fprintf(solu, ">>%05d", (int)(Weeksec - Beginsec) / 30 + 1);
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}
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}return 0;
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}
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+2
-3
@@ -169,9 +169,8 @@ FILE* headerout(pobs_head obs_h, int mode,
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FILE* result_file = fopen(res_path, "a+");
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fprintf(result_file, ">GENERATE PROGRAM : KNZ_GeoTrackLab ver%s\n", KNZ_GTL_VER);
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fprintf(result_file, " GENERATE SOURCE : %.10s\n", obs_h->marker);
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if (mode != 1); fprintf(result_file, " GENERATE TYPE : Position Resolve\n");
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if (mode == 0); fprintf(result_file, " GENERATE TYPE : Satellite Position\n");
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if (mode == 0); fprintf(result_file, " GENERATE TYPE : Position Resolve\n");
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if (mode == 1); fprintf(result_file, " GENERATE TYPE : Satellite Position\n");
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fprintf(result_file, " GENERATE TIME : %s", ctime(&gen_time));
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fprintf(result_file, " OBS FILE PATH : %s\n", obs_path);
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fprintf(result_file, " NAV FILE PATH : %s\n", nav_path);
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