Analysis of earth orbit rendezvous in terms of maneuver geometry served as basis for establishing requirements for visually sensed rendezvous guidance information; analysis of physical environment supported evaluation of sensory basis; visual capabilities were examined in terms of sensitivity, cross range motion perception, range, and range rate determinations; estimates of sensitivity and variability are presented where available; conclusions are drawn regarding adequacy of available data, and are given for future areas of study. (11037)
Visual sensing of spacecraft guidance information -- Earth orbit rendezvous maneuvers
NASA CR
NASA Contractor Reports ; n 1214;n 1214
1968
245 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Lyapunov-based Spacecraft Rendezvous Maneuvers using Differential Drag
British Library Conference Proceedings | 2011
|