Test failed, hopefully fixing
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@@ -17,8 +17,8 @@
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final = prop(thrust, start, test_sc, revs*T, Earth)[2]
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new_T = 2π * √( xyz_to_oe(final, Earth.μ)[1]^3 / Earth.μ )
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# This should be close enough to converge
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thrust_guess = spiral(0.88, n, start, test_sc, revs*T, Earth)
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# This should be close enough to converge, but Earth orbits are picky
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thrust_guess = spiral(0.89, n, start, test_sc, revs*T, Earth)
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result = solve_phase(start, final, test_sc, revs*T, thrust_guess, Earth)
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calc_path, calc_final = prop(result.zero, start, test_sc, revs*T, Earth, interpolate=true)
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