Pages that link to "Item:Q393657"
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The following pages link to A special case of spacecraft optimal attitude control (Q393657):
Displaying 40 items.
- On optimal spacecraft damping (Q357006) (← links)
- Optimal geometric motion planning for a spin-stabilized spacecraft (Q450675) (← links)
- The problem of optimal control of the orientation of an orbit of a spacecraft as a deformable figure (Q734022) (← links)
- Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft (Q734154) (← 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 on-off attitude control for the Brazilian multimission platform satellite (Q966286) (← links)
- Long time missions and the fuel-optimal attitude maneuvering in a swinging mode (Q1016346) (← links)
- Optimal reorientation of underactuated spacecraft using genetic algorithm with wavelet approximation (Q1049644) (← links)
- Optimal control on Lie groups with applications to attitude control (Q1272557) (← 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)
- Switching time-optimal control of spacecraft equipped with reaction wheels and gas jet thrusters (Q1642343) (← links)
- Quadratic optimal control in reorienting a spacecraft in a fixed time period in a dynamic problem statement (Q1647463) (← links)
- Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral method (Q1674152) (← links)
- On the problem of optimal spacecraft attitude control (Q1743047) (← links)
- Terminal synthesis of orbital orientation for a spacecraft (Q1745868) (← links)
- Design of the suboptimal profiled relay control of orientation of the spacecraft having elastic structural elements with regard for two oscillation tones (Q1778637) (← links)
- Analytic controlling reorientation of a spacecraft using a combined criterion of optimality (Q1795632) (← links)
- Attitude maneuvers which avoid a forbidden direction (Q1850846) (← links)
- Arbitrary fuel-optimal attitude maneuvering of a non-symmetric space vehicle in a vehicle-fixed coordinate frame (Q1868067) (← links)
- Optimal control of the orientation of systems of rigid and deformable bodies in a central field of force (Q1901549) (← links)
- Analysis of optimal motion control for a material point in a central field with application of quaternions (Q2017485) (← links)
- Minimum-time spacecraft attitude motion planning using objective alternation in derivative-free optimization (Q2055362) (← links)
- Energy optimal attitude control for a solar-powered spacecraft (Q2068599) (← links)
- Optimal control of a spacecraft orientation taking into account the energy of rotation (Q2226142) (← links)
- Analytical solution of a linear quadratic optimal control problem with control value constraints (Q2263872) (← 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 a rigid spacecraft programmed motion without angular velocity measurements (Q2432826) (← links)
- Optimal control of a programmed motion of a rigid spacecraft using redundant kinematics parameterizations (Q2484699) (← links)
- Optimal control of the angular momentum for a solid (spacecraft) performing a spatial turn (Q2699168) (← links)
- Time-optimal reorientation of the rigid spacecraft using a pseudospectral method integrated homotopic approach (Q2793927) (← links)
- Analysis of the inertially symmetric rigid spacecraft time-optimal three-axis reorientation (Q2965295) (← links)
- (Q3033374) (← links)
- Optimal non-linear feedback regulation of spacecraft angular momentum (Q3340584) (← links)
- Optimal nonlinear feedback control for spacecraft attitude maneuvers (Q3728750) (← links)
- Optimal stabilization of spacecraft in an inertial coordinate system based on a strapdown inertial navigation system (Q4961690) (← links)
- A Parameter Dependent Spacecraft Guidance Boundary Value Problem (Q5630572) (← 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)
