Spaceflight mechanics 1991; Proceedings of the 1st AAS/AIAA Annual Spaceflight Mechanics Meeting, Houston, TX, Feb. 11-13, 1991. Pts. 1 & 2

Computer Science – Performance

Scientific paper

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Astrodynamics, Attitude Control, Conferences, Interplanetary Trajectories, Large Space Structures, Orbital Mechanics, Aerocapture, Earth-Mars Trajectories, Flexible Spacecraft, Lunar Trajectories, Manned Mars Missions, Orbit Decay, Reentry Trajectories, Satellite Interceptors, Satellite Perturbation, Shape Control, Space Navigation, Space Station Freedom, Tethered Satellites, Trajectory Optimization, Vibration Damping

Scientific paper

Various papers on spaceflight mechanics are presented. Among the individual topics addressed are: eccentricity perturbations on a long tumbling dumbbell satellite, accurate and efficient tool for both lifetime predictions, minimizing deorbit maneuvers by hodographic analysis, autonomous optimal deorbit targeting, autonomous precision landing using terrain-following navigation, estimate of the global minimum DV needed for earth-moon transfer, architecting a mission plan for Lunar Observer, lunar cycler orbits with alternating semimonthly transfer windows, robotic precursor strategy for Mars exploration, onboard preaerocapture navigation performance at Mars, autonomous Mars sascent and orbit rendezvous for earth return missions. Also discussed are: free return trajectories for Mars missions, angular momentum and multibody dynamics, nutational stability and core energy of a quasi-rigid gyrostat, effect of moving mass on the Space Station Attitude Control System, motion requirements for antennas in geostationary earth orbit, shape control of flexible space structures, attitude control and momentum management of the Space Station. (For individual items see A93-17902 to A93-17970)

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