Solution of optimal-control problems for atmospheric entry

Details Solution of optimal-control problems for atmospheric entry Solution of optimal-control problems for atmospheric entry

Jan 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987kosis..25...37g&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 25, Jan.-Feb. 1987, p. 37-46. In Russian.

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Applications

Atmospheric Entry, Optimal Control, Spacecraft Reentry, Earth Atmosphere, Iterative Solution, Linearization, Trajectory Analysis

Scientific paper

A modified method of successive linearization is proposed which makes it possible to realize an iterative optimal-control search procedure in a class of piecewise-constant and continuous piecewise-linear functions. This modified method serves as the functional basis of an applications package intended to solve a large number of optimal-control problems involving spacecraft entry into planetary atmospheres. Attention is given to the determination of the attainability region and to the definition of a range of possible final velocities for atmospheric-entry trajectories leading to a prescribed point.

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