Control of spacecraft with relay-impulse and continuous-action controllers on the basis of an algorithm with a predictive model and its application to spacecraft rendezvous dynamics

Details Control of spacecraft with relay-impulse and continuous-action controllers on the basis of an algorithm with a predictive model and its application to spacecraft rendezvous dynamics Control of spacecraft with relay-impulse and continuous-action controllers on the basis of an algorithm with a predictive model and its application to spacecraft rendezvous dynamics

Mar 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27..206z&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, Mar.-Apr. 1989, p. 206-213. In Russian.

Mathematics

Control Theory, Prediction Analysis Techniques, Space Rendezvous, Spacecraft Control, Algorithms, Mathematical Models, Matrices (Mathematics), Optimal Control

Scientific paper

The paper examines the problem of spacecraft control with simultaneously functioning relay-impulse and continuous-action controllers using a modified optimal control algorithm with a predictive model reproducing the motion of the vehicle in accelerated time. The proposed theory is applied to the control of spacecraft rendezvous in an orbital coordinate system.

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