Synthesis of an algorithm of motion control in the vertical plane of a space shuttle vehicle at the stage of landing approach and flattening out

Details Synthesis of an algorithm of motion control in the vertical plane of a space shuttle vehicle at the stage of landing approach and flattening out Synthesis of an algorithm of motion control in the vertical plane of a space shuttle vehicle at the stage of landing approach and flattening out

Mar 1982

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1982kosis..20..206z&link_type=abstract

Kosmicheskie Issledovaniia, vol. 20, Mar.-Apr. 1982, p. 206-210. In Russian.

Physics

Approach Control, Control Theory, Space Shuttles, Spacecraft Guidance, Spacecraft Landing, Terminal Guidance, Algorithms, Differential Equations, Feedback Control, Time Dependence

Scientific paper

Feedback control laws for motion in the vertical plane of a space
shuttle vehicle during the approach and flattening-out stage are
developed on the basis of the inverse dynamics problem. Values of
control actions are determined from the solution of a first-order
differential equation.

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