Approximate analytical method for calculating the trajectories of a spacecraft with a working engine in an atmosphere

Details Approximate analytical method for calculating the trajectories of a spacecraft with a working engine in an atmosphere Approximate analytical method for calculating the trajectories of a spacecraft with a working engine in an atmosphere

Jul 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27..520s&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, July-Aug. 1989, p. 520-527. In Russian.

Statistics

Computation

Descent Trajectories, Spacecraft Reentry, Trajectory Optimization, Differential Equations, Error Analysis

Scientific paper

An approximate method for calculating spacecraft trajectories in an
atmosphere with allowance for rocket-dynamic forces is proposed. The
calculation error and length of computations are assessed, and the
results are illustrated by a number of numerical examples.

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