The problem of controlled spacecraft entry into an atmosphere

Details The problem of controlled spacecraft entry into an atmosphere The problem of controlled spacecraft entry into an atmosphere

Jul 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981kosis..19..634k&link_type=abstract

Kosmicheskie Issledovaniia, vol. 19, July-Aug. 1981, p. 634-638. In Russian.

Other

Atmospheric Entry, Ballistic Trajectories, Planetary Atmospheres, Spacecraft Control, Spacecraft Reentry, Aerodynamic Coefficients, Bessel Functions, Equations Of Motion, Spacecraft Motion

Scientific paper

The ballistic descent of a stabilized spacecraft in an atmosphere is analyzed with a view to deriving controlled motions which, through proper control, would imitate the uncontrolled motions. Conditions of dynamic stability are obtained for an axisymmetric spacecraft. The results can be used for theoretical modeling of the controlled imitation motions of spacecraft in the atmospheres of the earth and other planets.

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