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- W815715650 abstract "Closed form expressions are derived for the position and velocity of a spacecraft during a finite burn using the method involving the theory of asymptotic expansion of the optimal impulsive solution. The small parameter is given by the reciprocal of the mass flow rate. The expansion is given in terms of the impulsive solution and holds up through third-order for the velocity and fourth-order for the position." @default.
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- W815715650 date "1972-03-01" @default.
- W815715650 modified "2023-09-27" @default.
- W815715650 title "Asymptotic expansion of an impulse for an optimal finite burn" @default.
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