Voyager 2 Uranus targeting strategy

Details Voyager 2 Uranus targeting strategy Voyager 2 Uranus targeting strategy

Aug 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986asdy.conf.1331c&link_type=abstract

IN: Astrodynamics 1985; Proceedings of the Conference, Vail, CO, August 12-15, 1985. Part 2 (A86-43201 20-12). San Diego, CA, Un

Computer Science

Performance

Flyby Missions, Spacecraft Trajectories, Trajectory Optimization, Uranus (Planet), Voyager 2 Spacecraft, Arrivals, Confidence Limits, Miranda, Mission Planning, Monte Carlo Method, Spacecraft Maneuvers

Scientific paper

One of the major challenges involved in the Voyager 2 Uranus flyby is to deliver the spacecraft to an appropriate aimpoint at the optimum time, so as to maximize the science return of the mission, while yet keeping propellant expenditure low. An unusual targeting strategy has been devised to satisfy these requirements. Its complexity arises from the great distance of the planet Uranus and the limited performance capabilities of Voyager. This selected strategy is developed in relation to a set of candidate strategies, mission requirements and shifting science objectives. The analysis of these candidates is conducted via a Monte Carlo simulation, the results of which yield data for the comparative evaluation and eventual and selection of the actual targeting strategy to be employed.

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