Pages that link to "Item:Q1745868"
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The following pages link to Terminal synthesis of orbital orientation for a spacecraft (Q1745868):
Displaying 6 items.
- Analytical algorithm for constructing the orbital orientation of a spacecraft with an incomplete measurement of the state vector components (Q786105) (← links)
- Construction of the initial deorbit region for landing at the given place (Q1745815) (← links)
- Refining the Earth orientation parameters onboard spacecraft: concept and information technologies (Q1995347) (← links)
- Optimal orientation control of a space vehicle with restrictions on the control and phase variables (Q2134326) (← links)
- Optimal control of the angular momentum for a solid (spacecraft) performing a spatial turn (Q2699168) (← links)
- Optimal control of the reorientation of a spacecraft in the given time with a quadratic performance criterion related to the control and phase variables (Q6178158) (← links)
