Pages that link to "Item:Q734154"
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The following pages link to Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft (Q734154):
Displaying 20 items.
- On optimal spacecraft damping (Q357006) (← links)
- A special case of spacecraft optimal attitude control (Q393657) (← 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)
- Constructing Pontryagin extremals for the optimal control problem of asteroid fly-by (Q1040516) (← links)
- Quadratic optimal control in reorienting a spacecraft in a fixed time period in a dynamic problem statement (Q1647463) (← 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)
- On the signs of pulses in the problems of optimal control with fixed ends of the trajectories (Q1778533) (← links)
- Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions (Q1795633) (← links)
- Optimal control of the orientation of systems of rigid and deformable bodies in a central field of force (Q1901549) (← links)
- Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional (Q1982863) (← links)
- Optimal orientation control of a space vehicle with restrictions on the control and phase variables (Q2134326) (← links)
- Optimal control of a spacecraft orientation taking into account the energy of rotation (Q2226142) (← links)
- Restricted quadratic optimal control of a spacecraft turning in a fixed time period (Q2290476) (← links)
- Optimal control of rigid body's rotation movement with a combined quality criterion (Q2290508) (← links)
- Kinematically optimal spacecraft attitude control (Q2515397) (← 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)
- Control of the rotation of a solid (spacecraft) with a combined optimality criterion based on quaternions (Q6180785) (← links)
