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タイトルSpaceflight mechanics 1992; Proceedings of the 2nd AAS/AIAA Meeting, Colorado Springs, CO, Feb. 24-26, 1992. Pts. 1 & 2
著者(英)Diehl, Roger E.; Boden, Daryl G.; Williamson, Walton E.; Schinnerer, Ralph G.
著者所属(英)Jet Propulsion Lab., California Inst. of Tech.
発行日1992-01-01
1992
言語eng
内容記述The present conference discusses topics in orbit determination, tethered satellite systems, celestial mechanics, guidance optimization, flexible body dynamics and control, attitude dynamics and control, Mars mission analyses, earth-orbiting mission analysis/debris, space probe mission analyses, and orbital computation numerical analyses. Attention is given to electrodynamic forces for control of tethered satellite systems, orbiting debris threats to asteroid flyby missions, launch velocity requirements for interceptors of short range ballistic missiles, transfers between libration-point orbits in the elliptic restricted problem, minimum fuel spacecraft reorientation, orbital guidance for hitting a fixed point at maximum speed, efficient computation of satellite visibility periods, orbit decay and reentry prediction for space debris, and the determination of satellite close approaches.
NASA分類ASTRONAUTICS (GENERAL)
レポートNO93A48426
権利Copyright


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