Pages that link to "Item:Q2023246"
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The following pages link to Full state constrained stochastic adaptive integrated guidance and control for STT missiles with non-affine aerodynamic characteristics (Q2023246):
Displaying 5 items.
- Fuzzy adaptive fault tolerant IGC method for STT missiles with time-varying actuator faults and multisource uncertainties (Q2291044) (← links)
- Integrated guidance and control with partial state constraints and actuator faults (Q2419345) (← links)
- Impact angle controlled integrated guidance and control with input and state constraints (Q6548576) (← links)
- Safe approaching control for spacecraft rendezvous with disturbances: a positive system approach (Q6578918) (← links)
- Predefined time fuzzy adaptive control for stochastic nonlinear systems with limited time interval output constraints (Q6658999) (← links)