Pages that link to "Item:Q2226142"
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The following pages link to Optimal control of a spacecraft orientation taking into account the energy of rotation (Q2226142):
Displaying 22 items.
- On optimal spacecraft damping (Q357006) (← links)
- A special case of spacecraft optimal attitude control (Q393657) (← links)
- Controlling space vehicle reorientation with minimal energy integral (Q544754) (← links)
- Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft (Q734154) (← 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)
- Synthesis of spacecraft reorientation algorithms using the concept of the inverse dynamic problem (Q880750) (← links)
- Optimal moving control for small rotations of a spacecraft. II: Optimal synthesis (Q1285328) (← links)
- Optimal moving control for small rotations of a spacecraft. I: Optimal control (Q1285338) (← 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)
- Analytic controlling reorientation of a spacecraft using a combined criterion of optimality (Q1795632) (← links)
- Optimal control of the orientation of systems of rigid and deformable bodies in a central field of force (Q1901549) (← links)
- On improving the maneuverability of a space vehicle managed by inertial executive bodies (Q1995363) (← links)
- Energy optimal attitude control for a solar-powered spacecraft (Q2068599) (← links)
- Minimal energy maneuvering control of a rigid spacecraft with momentum transfer (Q2382768) (← links)
- Special control regime in the problem of optimal turn of an axially symmetric spacecraft (Q2391519) (← links)
- The optimal in terms of fuel consumption approach to reorientation of a spacecraft based on the nonlinear boundary value problem solution (Q2679185) (← links)
- Optimal non-linear feedback regulation of spacecraft angular momentum (Q3340584) (← links)
- Optimal Reorientation Of Spacecraft Orbit (Q3453359) (← links)
- Optimal Attitude Control with Two Rotation Axes (Q4630578) (← links)
- Optimal stabilization of spacecraft in an inertial coordinate system based on a strapdown inertial navigation system (Q4961690) (← links)
