Abstract
AbstractThe paper focuses on the automatic control of aircraft in the lateral‐directional plane during the landing approach phase, taking into account crosswind and sensor errors. Two new automatic landing systems are designed using the H‐inf control, dynamic inversion, optimal observers, and reference models. To validate them, we use the dynamics associated with the landing of a light airplane, we software implement the theoretical results, and analyze the accuracy of the results and the precision standards’ achievement with respect to the requirements of the Federal Aviation Administration for lateral error during the lateral‐directional motion of the aircraft during the landing approach phase.
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