Pages that link to "Item:Q361059"
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The following pages link to Integrated guidance and control for dual-control missiles based on small-gain theorem (Q361059):
Displaying 9 items.
- Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception (Q325728) (← links)
- Stabilizing region of \(PD^\mu\) controller for fractional order system with general interval uncertainties and an interval delay (Q1661265) (← links)
- Integrated aircraft control for rendezvous of aircraft-launched missiles with radiating targets (Q2263897) (← links)
- Integrated guidance and control with partial state constraints and actuator faults (Q2419345) (← 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)
- Adaptive Integrated Guidance and Control Based on Backstepping and <scp>I</scp>nput‐to‐<scp>S</scp>tate <scp>S</scp>tability (Q5420189) (← links)
- Neural learning control of missile interception against dynamics uncertainty and target evasive maneuver (Q6190230) (← links)
- Integrated guidance and control based on nonlinear model predictive control with simplified primal-dual neural network optimization (Q6611406) (← links)
