A two-stage solver with analytical warm-start and 1D refinement produces feasible guidance parameters for polynomial look-angle shaping that match open-loop optimal performance in tested UAV scenarios.
New Impact Time and Angle Guidance Strategy via Virtual Target Approach,
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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.
citing papers explorer
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Nonlinear Guidance for Arrival Time and Arrival Angle Control Using Trajectory Shaping
A two-stage solver with analytical warm-start and 1D refinement produces feasible guidance parameters for polynomial look-angle shaping that match open-loop optimal performance in tested UAV scenarios.
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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.