Investigation of the optimal two-parameter control of a spacecraft moving in an atmosphere

Details Investigation of the optimal two-parameter control of a spacecraft moving in an atmosphere Investigation of the optimal two-parameter control of a spacecraft moving in an atmosphere

Jan 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27...64s&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, Jan.-Feb. 1989, p. 64-70. In Russian.

Physics

Atmospheric Entry, Control Theory, Optimal Control, Spacecraft Control, Boundary Conditions, Boundary Value Problems, Differential Equations, Functionals

Scientific paper

The optimal control of a spacecraft in a planetary atmosphere is examined theoretically. The structure of two-parameter control is defined for problems with different optimized functionals and boundary conditions. In particular, expressions are presented which define the structure of the optimal control of attack and roll angles for two variational problems.

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