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Sep 03, 2024
- Delete de430.bsp · 43c5ba7b
  Thomas West authored 8 months ago
  
  43c5ba7b
- Total Delta V calculations for the Earth to Mars transfer using a lunar gravity assist. · d6034cb1
  Thomas West authored 8 months ago
  
  d6034cb1
- Delete Total_Delta_V_Lunar_Assist.m · 913d4b1d
  Thomas West authored 8 months ago
  
  913d4b1d
- Propagated orbit trajectory between Earth and Mars in heliocentric frame. · f13d4bb5
  Thomas West authored 8 months ago
  
  f13d4bb5
- Iterative solution to optimise lunar gravity assist and V-infinity globe calculations. · 894fb6be
  Thomas West authored 8 months ago
  
  894fb6be
- Total Delta V calculations for the Earth to Mars transfer using no lunar gravity assist. · 0a7dbd6d
  Thomas West authored 8 months ago
  
  0a7dbd6d
- Total Delta V calculations for the Earth to Mars transfer using no lunar gravity assist. · 03491c96
  Thomas West authored 8 months ago
  
  03491c96
- Mars capture orbit. · 4a0bd363
  Thomas West authored 8 months ago
  
  4a0bd363
- Optimal trajectory calculations between Earth parking orbit and leaving the SOI. · 73a9b350
  Thomas West authored 8 months ago
  
  73a9b350
- Porkchop plots for the 2024-2028 launch window. · 0d6f8ce1
  Thomas West authored 8 months ago
  
  0d6f8ce1
- MATLAB code for aerobraking calculations. · 88f3a68c
  Thomas West authored 8 months ago
  
  88f3a68c
- Animation showing the changes in orbit for a spacecraft performing aerobraking manoeuvres. · 018be0c2
  Thomas West authored 8 months ago
  
  018be0c2
- Function to calculate the true anomaly of a satellite around an orbit. · fbabbca0
  Thomas West authored 8 months ago
  
  fbabbca0
- Function to propagate the spacecraft orbit using 2 body problem theorem. · b9895857
  Thomas West authored 8 months ago
  
  b9895857
- Lambert solver using universal variables, to calculate orbits off all conic orbits. · a358a3cb
  Thomas West authored 8 months ago
  
  a358a3cb
- Kepler function. · 5e792d5e
  Thomas West authored 8 months ago
  
  5e792d5e
- Geometry and orbital coefficient calculations for an orbit. · de208b1d
  Thomas West authored 8 months ago
  
  de208b1d
- Cursor function when studying .mat figures. · 60ebf52d
  Thomas West authored 8 months ago
  
  60ebf52d
- Cursor function when studying .mat figures. · e078bf28
  Thomas West authored 8 months ago
  
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- Orbital coefficients to ECI frame · ec315925
  Thomas West authored 8 months ago
  
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- Calculation of semi-major axis with different variables. · d30bf6cd
  Thomas West authored 8 months ago
  
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- Lambert Solver Final Position when leaving the SOI of a body. · 5e7f1c02
  Thomas West authored 8 months ago
  
  5e7f1c02
- Delta V calculation for Pork Chop Plots · 46f32636
  Thomas West authored 8 months ago
  
  46f32636
- ephemeris data · e598a8ad
  Thomas West authored 8 months ago
  
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- matlab toolkit · 9aaffc8f
  Thomas West authored 8 months ago
  
  9aaffc8f
- Generic Kernels · f2f40fbf
  Thomas West authored 8 months ago
  
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- Animation for the transfer trajectory between Earth and Mars · 02906c76
  Thomas West authored 8 months ago
  
  02906c76
- Animation of the orbits of Earth and Mars · 1f1b3163
  Thomas West authored 8 months ago
  
  1f1b3163
- NASA Spice Toolkit used for ephemeris data of celestial bodies. · c09fa738
  Thomas West authored 8 months ago
  
  c09fa738
- The functions in this repository support iterative calculations. · bfedad2f
  Thomas West authored 8 months ago
  
  bfedad2f
- Trajectories of Earth and Mars around the Sun. · d81cf4fe
  Thomas West authored 8 months ago
  
  d81cf4fe
- Initial commit · b6a061da
  Thomas West authored 8 months ago
  
  b6a061da