Algorithm for turning a spacecraft with elastic elements at a given angle

Details Algorithm for turning a spacecraft with elastic elements at a given angle Algorithm for turning a spacecraft with elastic elements at a given angle

Oct 1974

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974kosis..12..797l&link_type=abstract

Kosmicheskie Issledovaniia, vol. 12, Sept.-Oct. 1974, p. 797-799. In Russian.

Computer Science

1

Airborne/Spaceborne Computers, Algorithms, Dynamic Models, Optimal Control, Spacecraft Control, Elastic Systems, Solar Cells, Spacecraft Guidance, Spacecraft Instruments, Steerable Antennas, Turning Flight

Scientific paper

Onboard computers can work out nearly optimal control algorithms for spacecraft by analysing the dynamic model of the craft; specific control parameters must be found in flight by application of a previously determined test program. Such a procedure is illustrated in the case of a spacecraft with elastic elements like antennas, solar batteries, etc. which must be turned at a prescribed angle in the plane of dynamic symmetry.

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