Multi-Step Optimization Strategy for Fuel-Optimal Orbital Transfer of Low-Thrust Spacecraft

An effective method for the design of fuel-optimal transfers in twoand threebody dynamics is presented. The optimal control problem is formulated using calculus of variation and primer vector theory. This leads to a multi-point boundary value problem (MPBVP), characterized by complex inner constraints and a discontinuous thrust profile. The first issue is addressed by embedding the MPBVP in a parametric optimization problem, thus allowing a simplification of the set of transversality constraints. The second problem is solved by representing the discontinuous control function by a smooth function depending on a continuation parameter. The resulting trajectory optimization method can deal with different intermediate conditions, and no a priori knowledge of the control structure is required. Test cases in both the twoand three-body dynamics show the capability of the method in solving complex trajectory design problems.