Pages that link to "Item:Q5420189"
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The following pages link to Adaptive Integrated Guidance and Control Based on Backstepping and <scp>I</scp>nput‐to‐<scp>S</scp>tate <scp>S</scp>tability (Q5420189):
Displaying 13 items.
- Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception (Q325728) (← links)
- Integrated guidance and control for dual-control missiles based on small-gain theorem (Q361059) (← links)
- Partial integrated missile guidance and control with state observer (Q490483) (← links)
- Full state constrained stochastic adaptive integrated guidance and control for STT missiles with non-affine aerodynamic characteristics (Q2023246) (← links)
- 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)
- Adaptive NN control of integrated guidance and control systems based on disturbance observer (Q2680252) (← links)
- Guidance laws with input constraints and actuator failures (Q2828570) (← links)
- Adaptive back-stepping sliding mode attitude control of missile systems (Q2857640) (← links)
- On an Optimized Fuzzy Supervized Multiphase Guidance Law (Q2960115) (← links)
- Robust partial integrated guidance and control approaches for maneuvering targets (Q3300465) (← links)
- Integrated interceptor guidance and control with prescribed performance (Q3458187) (← links)
- Integrated guidance and control of elastic flight vehicle based on robust MPC (Q3465695) (← links)
