Pages that link to "Item:Q786106"
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The following pages link to Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality (Q786106):
Displaying 13 items.
- Analytical algorithm for constructing the orbital orientation of a spacecraft with an incomplete measurement of the state vector components (Q786105) (← links)
- Synthesis of spacecraft reorientation algorithms using the concept of the inverse dynamic problem (Q880750) (← links)
- Synthesis of spacecraft covariance controls (Q895307) (← links)
- Terminal synthesis of orbital orientation for a spacecraft (Q1745868) (← links)
- Analytic controlling reorientation of a spacecraft using a combined criterion of optimality (Q1795632) (← links)
- Objects changing the spatial orientation of a solid body by using mobile mass (Q1995348) (← links)
- On improving the maneuverability of a space vehicle managed by inertial executive bodies (Q1995363) (← links)
- Control of a moving mass with the initial and final position on the boundary of the area of motion in order to achieve the fastest rotation of a solid body (Q2239211) (← links)
- Analytical quasi-optimal solution of the problem of the time-optimal rotation of a spacecraft (Q2239226) (← links)
- (Q3202766) (← links)
- (Q4798460) (← links)
- Improved guidance algorithm considering terminal attitude constraints for spacecrafts via optimal control theory (Q5003567) (← links)
- Analytical quasi-optimal algorithm for the programmed control of the angular motion of a spacecraft (Q6178157) (← links)
