Pages that link to "Item:Q2965295"
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The following pages link to Analysis of the inertially symmetric rigid spacecraft time-optimal three-axis reorientation (Q2965295):
Displaying 4 items.
- Near-minimum-time control of asymmetric rigid spacecraft using two controls (Q466284) (← links)
- Switching time-optimal control of spacecraft equipped with reaction wheels and gas jet thrusters (Q1642343) (← links)
- Time optimal control laws for bilinear systems (Q1721049) (← links)
- Time-optimal reorientation of the rigid spacecraft using a pseudospectral method integrated homotopic approach (Q2793927) (← links)