Asymptotic Behavior of Time Optimal Orbital Transfer for Low Thrust 2-body Control System
نویسندگان
چکیده
In the studies of low thrust time optimal orbital transfer it was conjectured that, when the thrust modulus tends to zero, the product of this modulus by the minimum transfer time admits a finite limit. The purpose of the present note is to better frame the nature of this asymptotic behavior and to prove this conjecture.
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