A First-Order Analytical Theory for Optimal Low-Thrust Limited-Power Transfers between Arbitrary Elliptical Coplanar Orbits

Table 1

Set of initial conditions and transfer duration.

	Set 1	Set 2
−0.0010	1.0	1.0
−0.0237	0.20	0.20
−0.0081	0.0	0.0
𝐽𝑓	8.5417×10^−5	4.2913×10^−5
8.6327×10^−5	4.3182×10^−5	8.6332×10^−5
4.3182×10^−5	0.0	0.0
𝑡𝑓−𝑡0=500	500	1000