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.
Generalized Impact Time and Angle Control Via Look-Angle Shaping,
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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.
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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.