A linear-quadratic optimal guidance law that enforces a terminal intercept angle under an explicit acceleration cap, with closed-form reachable-angle bounds, outperforms unconstrained laws when saturation occurs.
Interception ang le control guidance using proportional navigation with error feedback
3 Pith papers cite this work, alongside 197 external citations. Polarity classification is still indexing.
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A two-layer sliding mode control architecture is proposed to achieve simultaneous terminal time and angle constraints in nonlinear intercept guidance for stationary and constant-velocity targets.
Distributed guidance laws for multi-UAV cooperative attack reduce surrounding area to achieve simultaneous arrival and collision avoidance using line-of-sight components, requiring only spanning-tree communication.
citing papers explorer
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Optimal Guidance with Terminal Intercept-Angle Constraints and Acceleration Bounds
A linear-quadratic optimal guidance law that enforces a terminal intercept angle under an explicit acceleration cap, with closed-form reachable-angle bounds, outperforms unconstrained laws when saturation occurs.
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Terminal Time and Angle-Constrained Nonlinear Intercept Guidance
A two-layer sliding mode control architecture is proposed to achieve simultaneous terminal time and angle constraints in nonlinear intercept guidance for stationary and constant-velocity targets.
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Design of distributed guidance laws for multi-UAV cooperative attacking a moving target based on reducing surrounding area
Distributed guidance laws for multi-UAV cooperative attack reduce surrounding area to achieve simultaneous arrival and collision avoidance using line-of-sight components, requiring only spanning-tree communication.