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Lunar Descent Trajectory

Lunar Descent Trajectory. February 5 th , 2009. Descent Trajectory. Goal Determine trajectory, attitude, burn time, range & altitude EOM Derivation Assumptions Moon/spacecraft system, spherical & does not rotate, point masses 2-D problem

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Lunar Descent Trajectory

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  1. Lunar Descent Trajectory February 5th, 2009 [John Aitchison] [Mission Ops]

  2. Descent Trajectory [John Aitchison] [Mission Ops] • Goal • Determine trajectory, attitude, burn time, range & altitude • EOM Derivation Assumptions • Moon/spacecraft system, spherical & does not rotate, point masses • 2-D problem • T/m varies only with changing propellant mass (no throttling)

  3. Useful Numbers [John Aitchison] [Mission Ops] • Variability with: • Vehicle Mass • Thrust Capability • Lunar Parking Orbit

  4. Code (pg. 1) [John Aitchison] [Mission Ops]

  5. Code (pg. 2) [John Aitchison] [Mission Ops]

  6. Code (pg. 3) [John Aitchison] [Mission Ops]

  7. Code (pg. 4) [John Aitchison] [Mission Ops]

  8. Coordinate System [John Aitchison] [Mission Ops]

  9. Coordinate System Definitions [John Aitchison] [Mission Ops]

  10. Assumptions [John Aitchison] [Mission Ops]

  11. Calculations (pg. 1) [John Aitchison] [Mission Ops]

  12. Calculations (pg. 2) [John Aitchison] [Mission Ops]

  13. Calculations (pg. 3) [John Aitchison] [Mission Ops]

  14. Calculations (pg. 4) [John Aitchison] [Mission Ops]

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