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NASA NTRS · Conference Paper

Modeling lateral acceleration effects on pilot performance

Published 2016-06-06 From Legacy CDMS 2 authors
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Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

Attendant to the direct side force maneuver of a Vectored Force Fighter is the transverse acceleration imposed on the pilot. This lateral acceleration (Gy), when combind with a positive Gz stress, is a potential source of pilot tracking performance impairment. A research effort to investigate these performance decrements includes experimental as well as anaytical pilot performance modeling using the Optimal Control Model.

Authors

  • Korn, J. Connecticut Univ.
  • Kleinan, D. L. Connecticut Univ.

Citation: Korn, J., Kleinan, D. L. (2016). Modeling lateral acceleration effects on pilot performance. Legacy CDMS. NASA NTRS ID 19820026182. https://ntrs.nasa.gov/citations/19820026182 ↗