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kristian jerpetjøn
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Hello everyone i am new to these forums
As a part of my master thesis i am trying to construct transfer orbits based on pathces of the restricted 3 body problem.
However i keep meeting several walls
One is how to calculate the optimal orbit from the Earth orbit to the sun Earth L1 point
The next is propagating this until it falls back towards the Earth then patch it to the Earth moon restricted problem and fall trough Earth moon L2 into a low lunar orbit
All help is welcome
I have the book from belbruno covering much of the math involved but i am having problems constructing a program from it.
As a part of my master thesis i am trying to construct transfer orbits based on pathces of the restricted 3 body problem.
However i keep meeting several walls
One is how to calculate the optimal orbit from the Earth orbit to the sun Earth L1 point
The next is propagating this until it falls back towards the Earth then patch it to the Earth moon restricted problem and fall trough Earth moon L2 into a low lunar orbit
All help is welcome
I have the book from belbruno covering much of the math involved but i am having problems constructing a program from it.