Rotary-Wing Flight Display Test and Evaluation

Paper #:
  • 1999-01-5609

Published:
  • 1999-10-19
Citation:
Newman, R., "Rotary-Wing Flight Display Test and Evaluation," SAE Technical Paper 1999-01-5609, 1999, https://doi.org/10.4271/1999-01-5609.
Author(s):
Pages:
16
Abstract:
In recent years, helicopter flight and mission information has migrated from conventional round mechanical dials mounted on the instrument panel to software-dependent head-mounted displays capable of showing many types of information. Test and evaluation techniques have not progressed commensurate with display technology. A formal test and evaluation program is proposed to ensure that new information displays support the pilot’s flight tasks. An outline of test requirements is presented for use in future flight display programs.
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