Pages that link to "Item:Q2308118"
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The following pages link to Distributed adaptive fault-tolerant attitude tracking of multiple flexible spacecraft on \(\mathrm{SO}(3)\) (Q2308118):
Displaying 17 items.
- Distributed input observer-based finite-time consensus for the leader-following multi-agent systems (Q776138) (← links)
- Distributed adaptive tracking control of multiple flexible spacecraft under various actuator and measurement limitations (Q1649936) (← links)
- Distributed robust attitude tracking of multiple spacecraft with disturbances and unmodelled dynamics (Q1667017) (← links)
- Distributed attitude control for multiple flexible spacecraft under actuator failures and saturation (Q1676853) (← links)
- Decentralized event-triggered finite-time attitude consensus control of multiple spacecraft under directed graph (Q2068226) (← links)
- Robust adaptive sliding mode tracking control for a rigid body based on Lie subgroups of \(\mathrm{SO}(3)\) (Q2090459) (← links)
- Fixed-time control for high-precision attitude stabilization of flexible spacecraft (Q2220082) (← links)
- Integrated event-triggered fault estimation and fault-tolerant control for discrete-time fuzzy systems with input quantization and incomplete measurements (Q2318741) (← links)
- Second-order sliding-mode on SO(3) and fault-tolerant spacecraft attitude control (Q2681357) (← links)
- Mean square bounded attitude coordination control of spacecraft formation with stochastic uncertainties (Q2687792) (← links)
- Distributed fault-tolerant control design for spacecraft finite-time attitude synchronization (Q2820448) (← links)
- Distributed attitude synchronization control for multiple flexible spacecraft without modal variable measurement (Q4583657) (← links)
- Finite‐time cooperative attitude control for leader‐follower spacecraft with fixed‐time observer (Q6061232) (← links)
- Robust fixed-time attitude stabilization control of flexible spacecraft with actuator uncertainty (Q6166296) (← links)
- Finite-time spacecraft attitude control under input magnitude and rate saturation (Q6166382) (← links)
- Event-triggered adaptive fault-tolerant vibration control for a flexible robotic manipulator based on the partial differential equation model (Q6496659) (← links)
- Reinforcement-learning-based predefined-time relative orbit-attitude control for spacecraft formation flying with connectivity preserving (Q6645994) (← links)