Pages that link to "Item:Q1795632"

The following pages link to Analytic controlling reorientation of a spacecraft using a combined criterion of optimality (Q1795632):

Displaying 22 items.

• On optimal spacecraft damping (Q357006) (← links)
• A special case of spacecraft optimal attitude control (Q393657) (← links)
• Analytical solution of the of optimal slew problem of a spherically symmetric spacecraft in the class of conical motions (Q393693) (← links)
• Controlling space vehicle reorientation with minimal energy integral (Q544754) (← links)
• Control of spatial reorientation of a spacecraft using the free trajectory method (Q740566) (← links)
• Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality (Q786106) (← links)
• Analytical quasi-optimal solution of the slew problem for an axially symmetric rigid body with a combined performance index (Q786160) (← links)
• Synthesis of spacecraft reorientation algorithms using the concept of the inverse dynamic problem (Q880750) (← links)
• Optimal reorientation of a Spacecraft's orbit using a jet thrust orthogonal to the orbital plane (Q900318) (← links)
• Quadratic optimal control in reorienting a spacecraft in a fixed time period in a dynamic problem statement (Q1647463) (← links)
• Threshold absolute value of a relay control when time-optimally bringing a satellite to a gravitationally stable position (Q1735290) (← links)
• On the problem of optimal spacecraft attitude control (Q1743047) (← links)
• Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions (Q1743200) (← links)
• Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional (Q1982863) (← links)
• On improving the maneuverability of a space vehicle managed by inertial executive bodies (Q1995363) (← links)
• Optimal control of a spacecraft orientation taking into account the energy of rotation (Q2226142) (← links)
• Optimal control of a programmed motion of a rigid spacecraft using redundant kinematics parameterizations (Q2484699) (← links)
• The optimal in terms of fuel consumption approach to reorientation of a spacecraft based on the nonlinear boundary value problem solution (Q2679185) (← links)
• Minimum time control of the rocket attitude reorientation associated with orbit dynamics (Q2796010) (← links)
• (Q3202766) (← links)
• Optimal stabilization of spacecraft in an inertial coordinate system based on a strapdown inertial navigation system (Q4961690) (← links)
• The new algorithm of quasi-optimal reorientation of a spacecraft (Q6488025) (← links)