Titlebook: Satellite Dynamics; Symposium São Paulo/ Girgio E. O. Giacaglia,A. C. Stickland Conference proceedings 1975 Springer-Verlag, Berlin/Heidelb

Gleason-score

The Rotational Motion of a Satellite and Atmospheric Density Determinationnt of aerodynamic pressure can produce an autorotation — a peculiar twisting of the satellite that causes an acceleration of the satellite’s spin. The spin can be also accelerated by the moment of aerogradient. The integration of the equation of satellite motion allowing for the moment of aerodynami

轻浮思想

On the Stability of Spinning Flexible Satellitesand in addition, new criteria depending essentially on the flexible properties of the system. Moreover, the influence of the number of the considered eigenfunctions is investigated with respect to the stability boundary.

效果

Aerate

facilitate

Intrepid

At a time where it might be thought that very few problems were left un­ solved in celestial mechanics, we discover that new and more challenging questions must be answered. The pre­ cision of observations reaches the centimeter level and physical phenomena which had been disregarded come into play.

interior

Analytical Theories of the Motion of Artificial Satellites. Most theories treat the main problem (i.e. problem of the oblateness perturbations), and they are classified according to a) intermediaries adopted, b) perturbation techniques used, and c) orders of approximations carried out. We next review the theories that treat of other sources of perturbation

Rustproof

Lucubrate

潜移默化

Importance of the Moon-Earth Coupling Effect in the Motion of an Artificial Satellite: Semi-Analyticand Moon one needs to consider coupling the effects not only by secular and long period terms, but also by short period terms. This has been computed and pointed out. We have also computed (and checked by analytical-numerical comparisons) a very effective semi-analytical solution of this problem and