Abstract
Abstract
Flightpath prediction can substantially enhance the guidance and control capabilities offered by a novel display type that presents guidance information in a three-dimensional format. Based on pilot-centred requirements, a predictor design for longitudinal motion is proposed to achieve minimum pilot compensation for controlling the predictor-aircraft system. Key configuration factors of the pilot-predictor-aircraft system are identified and optimized. The compensatory control issues are verified in a simulation test program.
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