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• W2150798519 abstract "This tutorial paper describes a high-level guidance algorithm based on model predictive control. The algorithm follows a precomputed flight plan (which provides a reference trajectory based on straight segments) by calculating the aerodynamic velocity, flight path angle and bank angle commands for a low level attitude controller. To compute these control signals, the guidance law uses a nonlinear 3DoF aircraft model for state prediction that leads to a nonlinear optimization problem, which is solved using a iterative scheme. The algorithm uses as a hotstart a robust missile guidance law, thus guaranteeing feasibility. Simulation results show the effectiveness of the proposed guidance law." @default.
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• W2150798519 date "2015-07-01" @default.
• W2150798519 modified "2023-10-07" @default.
• W2150798519 title "A High-level model predictive control guidance law for unmanned aerial vehicles" @default.
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• W2150798519 doi "https://doi.org/10.1109/ecc.2015.7330728" @default.
• W2150798519 hasPublicationYear "2015" @default.
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