An interplanetary targeting and orbit insertion maneuver design technique

Details An interplanetary targeting and orbit insertion maneuver design technique An interplanetary targeting and orbit insertion maneuver design technique

Aug 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980aiaa.confz....h&link_type=abstract

American Institute of Aeronautics and Astronautics and American Astronautical Society, Astrodynamics Conference, Danvers, Mass.,

Astronomy and Astrophysics

Astronomy

Interplanetary Navigation, Orbital Maneuvers, Spacecraft Control, Spacecraft Maneuvers, Angle Of Attack, Attitude Control, Celestial Reference Systems, Orbit Calculation, Pioneer Venus 1 Spacecraft, Real Time Operation, Target Acquisition, Trajectory Control

Scientific paper

The paper describes a tradeoff in selecting a planetary encounter aimpoint and a spacecraft propulsive maneuver strategy in the Pioneer Venus Orbiter Mission. The method uses parametric data spanning a region of acceptable targeting aimpoints in the delivery space and the geometric considerations. Real-time maneuver adjustments accounted for known attitude control errors, orbit determination updates, and late changes in a targeting specification.

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