Researchers simplified the analytical expression of the line of sight (LOS) error, discovered and proved the independence of Euler angle Psi, calculated attitude angles corresponding to 0 degrees and 20 degrees LOS errors, determined choices of initial alignment, tailored the slew maneuvers for LOS pointing, simulated numerically the LOS pointing slew of the Spacecraft Control Laboratory Experiment (SCOLE), and evaluated the pointing performance.
Rapid torque-bounded line-of-sight pointing of SCOLE with a designer's choice of initial alignment
1984-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Optimal torque control for SCOLE slewing maneuvers
NTRS | 1987
|On-line identification and attitude control for SCOLE
AIAA | 1987
|