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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Spaceflight mechanics 1992; Proceedings of the 2nd AAS/AIAA Meeting, Colorado Springs, CO, Feb. 24-26, 1992. Pts. 1 & 2


    Contributors:

    Publication date :

    1992-01-01




    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    23rd AAS/AIAA Spaceflight Mechanics Meeting

    American Institute of Aeronautics and Astronautics / American Astronautical Society | DataCite | 2013



    Spaceflight mechanics 1999 : proceedings of the AAS/AIAA Space Flight Mechanics Meeting held February 7 - 10, 1999, Breckenridge, Colorado / ed. by Robert H. Bishop ... ; Pt. 2

    Space Flight Mechanics Meeting / American Astronautical Society / American Institute of Aeronautics and Astronautics | TIBKAT | 1999