Pages that link to "Item:Q2205461"
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The following pages link to Integrated fault tolerant tracking control for rigid spacecraft using fractional order sliding mode technique (Q2205461):
Displaying 10 items.
- Barrier Lyapunov function-based adaptive fuzzy attitude tracking control for rigid satellite with input delay and output constraint (Q2058007) (← links)
- Fault-tolerant control for the linearized spacecraft attitude control system with Markovian switching (Q2096114) (← links)
- Solving a reliability-performance balancing problem for control systems with degrading actuators under model predictive control framework (Q2148451) (← links)
- Integrated fault tolerant attitude control approach for satellite attitude system with sensor faults (Q5000766) (← links)
- Extended state observer-based attitude fault-tolerant control of rigid spacecraft (Q5027775) (← links)
- Adaptive saturated tracking control for spacecraft proximity operations via integral terminal sliding mode technique (Q6082381) (← links)
- Prescribed performance adaptive fault tolerant control approach for nonlinear large‐scale systems with time delay interconnection and dead zone input (Q6092337) (← links)
- Sliding mode control‐based distributed fault tolerant tracking control for multiple unmanned aerial vehicles with input constraints and actuator faults (Q6194760) (← links)
- An adaptive sliding mode fault‐tolerant control of a quadrotor unmanned aerial vehicle with actuator faults and model uncertainties (Q6194829) (← links)
- Refined fault tolerant tracking control of fixed-wing UAVs via fractional calculus and interval type-2 fuzzy neural network under event-triggered communication (Q6492067) (← links)
