Pages that link to "Item:Q2793927"
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The following pages link to Time-optimal reorientation of the rigid spacecraft using a pseudospectral method integrated homotopic approach (Q2793927):
Displaying 4 items.
- Pseudospectral method based trajectory optimization and fairing rejection time analysis of solid launch vehicle (Q1047425) (← links)
- Bang-bang optimal control for differentially flat systems using mapped pseudospectral method and analytic homotopic approach (Q2835503) (← links)
- Analysis of the inertially symmetric rigid spacecraft time-optimal three-axis reorientation (Q2965295) (← links)
- Improved guidance algorithm considering terminal attitude constraints for spacecrafts via optimal control theory (Q5003567) (← links)