Computation, details, computer listings, graphs, and tables are presented for the investigation into flexure-satellite attitude interaction due to two uniform beam arrays on a three axis stabilized spacecraft.
Attitude Control of Three-Axes Stabilized Spacecraft with Flexible Appendages, Volume 2
1977
240 pages
Report
Keine Angabe
Englisch
Unmanned Spacecraft , Spacecraft Trajectories & Flight Mechanics , Appendages , Flexible bodies , Satellite attitude control , Three axis stabilization , Computer programs , Feedback control , Gimbals , Graphs (Charts) , Modal response , Reaction wheels , Solar arrays , Tables (Data) , Torque , Transfer functions , Transient response , Great Britain
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