Orbital maneuver optimization using time-explicit power series

Details Orbital maneuver optimization using time-explicit power series Orbital maneuver optimization using time-explicit power series

May 2011

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2011cemda.110...31t&link_type=abstract

Celestial Mechanics and Dynamical Astronomy, Volume 110, Issue 1, pp.31-42

Astronomy and Astrophysics

Astronomy

Orbital Maneuver Optimization, Lambert Problem, Orbital Mission Planning, Thorne Series Solution Of Lambert Problem

Scientific paper

Orbital maneuver transfer time optimization is traditionally accomplished using direct numerical sampling to find the mission design with the lowest delta-v requirements. The availability of explicit time series solutions to the Lambert orbit determination problem allows for the total delta-v of a series of orbital maneuvers to be expressed as an algebraic function of only the individual transfer times. The delta-v function is then minimized for a series of maneuvers by finding the optimal transfer times for each orbital arc. Results are shown for the classical example of the Hohmann transfer, a noncoplanar transfer as well as an interplanetary fly-by mission to the asteroids Pallas and Juno.

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