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Optimal Design of a Mission to Neptune

For an interplanetary spacecraft from the Earth to the planet of Neptune trajectory optimization and the optimization of spacecraft design are tightly coupled to increase overall system performance.

R. Callies | R. Callies

[1] M. Hestenes. Calculus of variations and optimal control theory , 1966 .

[2] J. Stoer,et al. Numerical treatment of ordinary differential equations by extrapolation methods , 1966 .

[3] M. R. Osborne. On shooting methods for boundary value problems , 1969 .

[4] P. Deuflhard. Ein Newton-Verfahren bei fastsingulärer Funktionalmatrix zur Lösung von nichtlinearen Randwertaufgaben mit der Mehrzielmethode , 1972 .

[5] Gary L. Bennett,et al. On the development of the power sources for the Ulysses and Galileo missions , 1989 .

[6] R. Callies,et al. Optimal trajectories for a multiple rendezvous mission to asteroids , 1991 .

[7] R. Brown. Triton - Voyager's finale , 1992 .