Pages that link to "Item:Q4014674"
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The following pages link to Time-optimal slewing of flexible spacecraft (Q4014674):
Displaying 9 items.
- Nonlinear attitude control scheme with disturbance observer for flexible spacecrafts (Q327838) (← links)
- Optimal limited-rate slewing of a flexible spacecraft (Q368354) (← links)
- An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts (Q437341) (← links)
- Optimal vibration control of flexible spacecraft during a minimum-time maneuver (Q757823) (← links)
- Nonlinear minimum-time control with pre- and post-actuation (Q2276106) (← links)
- Nonlinear feedback control of slewing beams (Q2495561) (← links)
- Frequency and Time Domain Analysis of an Aeroelastic Wing Multiple Component Structure (Q3453799) (← links)
- SPACE-TIME SPECTRAL ELEMENT METHOD FOR OPTIMAL SLEWING OF A FLEXIBLE BEAM (Q4344910) (← links)
- Time‐energy optimal control of vector controlled induction motor (Q4537266) (← links)