Pages that link to "Item:Q1956927"

The following pages link to Special control regime in optimal turn problem of spherically symmetric spacecraft (Q1956927):

Displaying 11 items.

• Analytical solution of the of optimal slew problem of a spherically symmetric spacecraft in the class of conical motions (Q393693) (← links)
• Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality (Q786106) (← links)
• Solution of the problem of the optimal turn of a spherically symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions (Q880847) (← links)
• Analytic controlling reorientation of a spacecraft using a combined criterion of optimality (Q1795632) (← links)
• A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions (Q1951950) (← links)
• On improving the maneuverability of a space vehicle managed by inertial executive bodies (Q1995363) (← links)
• Special control mode in the problem of optimal turn of an arbitrary rigid body (spacecraft) (Q2263415) (← links)
• Analytical solution of the time-optimal slew problem of a spherically symmetric spacecraft in the class of conical motions (Q2263885) (← links)
• Restricted quadratic optimal control of a spacecraft turning in a fixed time period (Q2290476) (← links)
• Special control regime in the problem of optimal turn of an axially symmetric spacecraft (Q2391519) (← links)
• Optimal control of the angular momentum for a solid (spacecraft) performing a spatial turn (Q2699168) (← links)