Pages that link to "Item:Q1622215"
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The following pages link to Backstepping-based adaptive dynamic programming for missile-target guidance systems with state and input constraints (Q1622215):
Displaying 18 items.
- Disturbance observer-based robust missile autopilot design with full-state constraints via adaptive dynamic programming (Q1661734) (← links)
- Approximate dynamic programming for missile defense interceptor fire control (Q1751900) (← links)
- Robust adaptive prescribed performance dynamic surface control for uncertain nonlinear pure-feedback systems (Q1989287) (← links)
- Terminal angle constraint finite-time guidance law with input saturation and autopilot dynamics (Q2094958) (← links)
- A nonlinear robust model predictive differential game guidance algorithm based on the particle swarm optimization (Q2205496) (← links)
- Adaptive neural torsional vibration suppression of the rolling mill main drive system subject to state and input constraints with sensor errors (Q2217608) (← links)
- Robust intercept guidance law with predesigned zero-effort miss distance convergence for capturing maneuvering targets (Q2291118) (← links)
- An improvement of single-network adaptive critic design for nonlinear systems with asymmetry constraints (Q2334181) (← links)
- A modified cooperative proportional navigation guidance law (Q2423980) (← links)
- Adaptive NN control of integrated guidance and control systems based on disturbance observer (Q2680252) (← links)
- Adaptive back-stepping sliding mode attitude control of missile systems (Q2857640) (← links)
- Finite-horizon differential games for missile–target interception system using adaptive dynamic programming with input constraints (Q4638033) (← links)
- An overview on the adaptive dynamic programming based missile guidance law (Q4642787) (← links)
- Event-triggered adaptive approximately optimal tracking control of a class of non-affine SISO nonlinear systems via output feedback (Q5029187) (← links)
- Zero-sum differential games-based fast adaptive robust optimal sliding mode control design for uncertain missile autopilot with constrained input (Q5095511) (← links)
- Distributed optimal event‐triggered cooperative control for nonlinear multi‐missile guidance systems with partially unknown dynamics (Q6090251) (← links)
- Overcoming backstepping limitations via a novel MIMO non-affine-in-control convex optimization technique (Q6177542) (← links)
- Appointed-time-control-based three-dimensional parallel approaching guidance for intercepting maneuvering target (Q6601169) (← links)
