Analytical estimates in problems of the nonlinear stabilization of a spacecraft during descent in the atmosphere

Details Analytical estimates in problems of the nonlinear stabilization of a spacecraft during descent in the atmosphere Analytical estimates in problems of the nonlinear stabilization of a spacecraft during descent in the atmosphere

Mar 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27..186p&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, Mar.-Apr. 1989, p. 186-192. In Russian.

Physics

Atmospheric Entry, Descent Trajectories, Space Flight, Spacecraft Stability, Atmospheric Stratification, Nonlinear Systems, Transient Response

Scientific paper

A differential equation for the transient process is obtained in the
general nonlinear formulation of the problem of spacecraft stabilization
during descent in the atmosphere. Conditions allowing the construction
of approximate analytical solutions are formulated. These solutions are
reduced to the case of an oscillatory transient process.

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