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Spaceflight mechanics 1992; Proceedings of the 2nd AAS/AIAA Meeting, Colorado Springs, CO, Feb. 24-26, 1992. Pts. 1 & 2The 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.
Document ID
19930064429
Document Type
Conference Proceedings
Authors
Diehl, Roger E. (JPL Pasadena, CA, United States)
Schinnerer, Ralph G. (Loral Command & Control Systems Colorado Springs, CO, United States)
Williamson, Walton E. (Sandia National Labs. Albuquerque, NM, United States)
Boden, Daryl G. (U.S. Air Force Academy Colorado Springs, CO, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
ISSN: 0065-3438
ISBN: 0065-3438
Subject Category
ASTRONAUTICS (GENERAL)
Distribution Limits
Public
Copyright
Other

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