8000 saintograph (Winfred) · GitHub
[go: up one dir, main page]
Skip to content
View saintograph's full-sized avatar
👾
Boop boop beep boop
👾
Boop boop beep boop
8 followers · 0 following

Achievements

Achievement: Pull Sharkx3Achievement: YOLOAchievement: Arctic Code Vault Contributor

Achievements

Achievement: Pull Sharkx3Achievement: YOLOAchievement: Arctic Code Vault Contributor

Block or report saintograph

Block user

Prevent this user from interacting with your repositories and sending you notifications. Learn more about blocking users.

You must be logged in to block users.

Please don't include any personal information such as legal names or email addresses. Maximum 100 characters, markdown supported. This note will be visible to only you.
Report abuse

Contact GitHub support about this user’s behavior. Learn more about reporting abuse.

Report abuse

Pinned Loading

  1. Radiated particle detection cloud ch... Radiated particle detection cloud chamber
    1 
    import cv2 as cv
    2 
    import imutils
    3 
    import PIL
    4 
    from PIL import Image, ImageEnhance
    5 
    from scipy.spatial import distance as dist
  2. Getting ground station coverage Getting ground station coverage
    1 
    # Load ground stations from CSV
    2 
    import pandas as pd
    3 
    import matplotlib.pyplot as plt
    4 
    import geopandas as gpd
    5 
    
              
    
          
    
    
    
  
    

    3. 

      

  3. 
  
    
    
    
      
    
        
        Deorbiting a satellite  Deorbiting a satellite      
    

          
    
              
    
                1
                
    % Define input parameters
    
              
    
              
    
                2
                
    Re = 6378.137;         % Earth Radius (km)
    
              
    
              
    
                3
                
    initial_altitude = 600; % Initial Altitude (km)
    
              
    
              
    
                4
                
    a = Re + initial_altitude; % Semi-Major Axis (km)
    
              
    
              
    
                5
                
    e = 0.001;             % Eccentricity
    
              
    
          
    
    
    
  
    

    4. 

      

  4. 
  
    
    
    
      
    
        
        Sun-synchronous orbit for 1U satelli...  Sun-synchronous orbit for 1U satellite at 600km      
    

          
    
              
    
                1
                
    % URSA-1 Sun-Synchronous Orbit Simulation
    
              
    
              
    
                2
                
    % Altitude: 600 km
    
              
    
              
    
                3
                
    % Inclination: ~97.8° (calculated for sun-synchronous condition)
    
              
    
              
    
                4
                
    % Eccentricity: 0.001
    
              
    
              
    
                5
                
    % RAAN: Calculated based on Berlin's location
    
              
    
          
    
    
    
  
    

    5. 












      
  
        

          
  
    
    

        

        

  





        

      





      

  


          



    



  

    

    

    





    

    

    

  


0