The MAST Flight System as a test bed for large space structure control algorithms is discussed. An overview is given of the control system architecture. The actuators, the sensors, the control computer, and the baseline damping algorithm are discussed.
Mast Flight System Dynamic Performance
1986
18 pages
Report
No indication
English
Unmanned Spacecraft , Manned Spacecraft , Beams (Supports) , Control systems design , Controllers , Large space structures , Structural vibration , Trusses , Vibration damping , Aerospace systems , Algorithms , Flexible bodies , Accelerometers , Actuators , Aerospace engineering , Computers , Electric motors , Space shuttles , Structural engineering , Torsion
MAST flight system dynamic performance
NTRS | 1986
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