I’m currently using the function stateToTLE() to convert an osculating orbit into a TLE and it works well.
I’ve read about issues for GEO, but since I am using it only for a LEO satellite, I should be fine.
My question is, if someone might be able to explain me how the function manages to approximate the mean orbit from the osculating orbit.
Specifically, how do these lines:
// update state sma += deltaSma; ex += deltaEx; ey += deltaEy; hx += deltaHx; hy += deltaHy; lv += deltaLv;
with the delta values being computed ahead like this:
// adapted parameters residuals final double deltaSma = equiOrbit.getA() - recovEquiOrbit.getA(); final double deltaEx = equiOrbit.getEquinoctialEx() - recovEquiOrbit.getEquinoctialEx(); final double deltaEy = equiOrbit.getEquinoctialEy() - recovEquiOrbit.getEquinoctialEy(); final double deltaHx = equiOrbit.getHx() - recovEquiOrbit.getHx(); final double deltaHy = equiOrbit.getHy() - recovEquiOrbit.getHy(); final double deltaLv = MathUtils.normalizeAngle(equiOrbit.getLv() - recovEquiOrbit.getLv(), 0.0);
make it work?
From how I’ve understood, it roughly works like this:
Step 1: initializes a TLEPropagator with the initial osculating orbit as a TLE, which returns an osculating orbit.
Step 2: compute delta values “initial_osculating_orbit - current_osculating_orbit”
Step 3: check if delta is lower than the set threshold and stop here if it’s the case.
Step 4: add delta values to the last osculating values (starting from the initial orbit).
Step 5: create a new TLE with the updated osculating orbit and use it as input for a new TLEPropagator, which returns a new osculating orbit. Redo steps 2 to 5 until convergence criteria is met.
So, somehow, we start with our initial osculating orbit as a “fake TLE”. And the more we iterate through our loop and add deltas to our initial osculating orbit, it becomes the mean orbit.
How comes, just adding these deltas makes it work? Is it based on a mathematical model and if so, which?
In the comments of the code, it says it uses Newton Iteration. But to be honest, I can’t identify Newton Iteration from this part.
Also, authors for the class TLE are Fabien Maussion and Luc Maisonobe. Do you think I could @ them here to ask them directly or should I rather not bother them…
As this function is basically the core of my Bachelor Thesis, which I am writing at the moment, I would like to understand the idea behind it and the mathematics. I am thankful for any advise or explanatory comments.