Pages that link to "Item:Q325728"
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The following pages link to Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception (Q325728):
Displaying 14 items.
- Integrated guidance and control for dual-control missiles based on small-gain theorem (Q361059) (← links)
- Dual control guidance for simultaneous identification and interception (Q760374) (← links)
- Integrated estimation/guidance law against exoatmospheric maneuvering targets (Q1723083) (← links)
- Integrated guidance and control with input saturation and impact angle constraint (Q2004187) (← links)
- Integrated aircraft control for rendezvous of aircraft-launched missiles with radiating targets (Q2263897) (← links)
- Adaptive NN control of integrated guidance and control systems based on disturbance observer (Q2680252) (← links)
- A novel three-dimensional guidance law implementation using only line-of-sight azimuths (Q2795779) (← links)
- (Q3196913) (← links)
- Robust partial integrated guidance and control approaches for maneuvering targets (Q3300465) (← links)
- Integrated 3‐D Flight Trajectory Tracking Control with Aerodynamic Constraints on Attitude and control Surfaces (Q4620345) (← links)
- (Q4623917) (← 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)
- A novel adaptive three-dimensional finite-time guidance law with terminal angle constraints for interception of maneuvering targets (Q5863740) (← links)
- Three-dimensional low-order fixed-time integrated guidance and control for STT missile with strap-down seeker (Q6053859) (← links)
