Pages that link to "Item:Q5416957"
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The following pages link to Optimal Output Feedback Controllers for Spacecraft Attitude Tracking (Q5416957):
Displaying 15 items.
- Optimal on-off attitude control for the Brazilian multimission platform satellite (Q966286) (← links)
- Inverse optimal control via diagonal stabilization applied to attitude tracking of a reusable launch vehicle (Q2055364) (← links)
- Optimal feedback gains determination method for nominal reentry guidance (Q2800477) (← links)
- The synthesis of the proportional-differential regulators for the systems with fixed ends of trajectories under two-sided constraints on control values (Q2821203) (← links)
- Adaptive fuzzy PD+ control for attitude maneuver of rigid spacecraft (Q2821218) (← links)
- Optimal Tracking for State-Dependent Coefficient Factorized Nonlinear Systems (Q2930780) (← links)
- On the Design of Observer for Nonlinear Time-Delay Systems (Q2930815) (← links)
- Output Feedback Control of Relative Translation in a Leader-Follower Spacecraft Formation (Q3016428) (← links)
- Optimal non-linear feedback regulation of spacecraft angular momentum (Q3340584) (← links)
- An optimal dynamic output feedback controller for a flexible spacecraft (Q3469023) (← links)
- Optimal nonlinear feedback control for spacecraft attitude maneuvers (Q3728750) (← links)
- (Q4921302) (← links)
- Reduced‐order Observer for State‐dependent Coefficient Factorized Nonlinear Systems (Q5215167) (← links)
- Two-layer terminal sliding mode attitude control of satellites equipped with reaction wheels (Q6563344) (← links)
- Finite-time adaptive fault-tolerant control for rigid spacecraft attitude tracking (Q6569875) (← links)
