Navigation system design for a Halley Flyby/Tempel 2 Rendezvous mission using ion drive

Details Navigation system design for a Halley Flyby/Tempel 2 Rendezvous mission using ion drive Navigation system design for a Halley Flyby/Tempel 2 Rendezvous mission using ion drive

Jun 1979

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979aiaa.confr....w&link_type=abstract

American Astronautical Society and American Institute of Aeronautics and Astronautics, Astrodynamics Specialist Conference, Prov

Astronomy and Astrophysics

Astronomy

Halley'S Comet, Mission Planning, Orbit Calculation, Satellite Guidance, Satellite Navigation Systems, Solar Electric Propulsion, Systems Engineering, Accuracy, Circular Orbits, Nasa Programs, Orbit Perturbation, Orbital Rendezvous, Satellite Orbits, Space Shuttles, Tables (Data)

Scientific paper

A dual comet (Hall Flyby/Tempel 2 Rendezvous) mission, making use of the solar electric propulsion system, is under consideration for a 1985 launch. This paper describes the preliminary navigation system design for this mission. Orbit determination and guidance strategies for each mission phase are discussed. Navigation accuracy analyses and parametric senstivity studies for the Tempel 2 rendezvous approach phase are presented.

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