Hoh Aeronautics, Inc. Research Update David G. Mitchell Technical Director 310-325-7280 dmitchell@hoh-aero.com - PowerPoint PPT Presentation

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Hoh Aeronautics, Inc. Research Update David G. Mitchell Technical Director 310-325-7280 dmitchell@hoh-aero.com

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Hoh Aeronautics, Inc. Research Update David G. Mitchell Technical Director 310-325-7280 dmitchell_at_hoh-aero.com SAE AC&GS Committee Meeting Williamsburg, VA – PowerPoint PPT presentation

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Title: Hoh Aeronautics, Inc. Research Update David G. Mitchell Technical Director 310-325-7280 dmitchell@hoh-aero.com


1
Hoh Aeronautics, Inc.Research UpdateDavid G.
MitchellTechnical Director310-325-7280dmitchell
_at_hoh-aero.com
  • SAE ACGS Committee Meeting
  • Williamsburg, VA
  • October 2006

2
Handling Qualities Requirements for Maritime,
Cargo, UAV Rotorcraft
  • Small Business Innovation Research Contracts from
    NAVAIR
  • Completed Phase I
  • Phase II expected to start early 2007
  • Working with Advanced Rotorcraft Technology
    (under a separate Phase II SBIR from NAVAIR)
  • Update ADS-33E-PRF requirements
  • Multiple flight and ground simulation programs
  • Produce ADS-33 Software Application Package

3
Research Facilities
  • Sikorsky simulator
  • ART simulator
  • NASA Ames VMS
  • NRC variable-stability Bell 205
  • Navy CH-53

4
Key Research Topic Nonlinearities
  • How do we deal with nonlinearities in frequency
    and time responses?
  • Cases to the right all looked the same to one
    pilot in a fixed-base simulator
  • Specs lack analysis techniques and guidance to
    the user for such cases
  • Nonlinearities are common in rotorcraft
  • Rotor/mast modes
  • Slung load modes
  • FCS limits and switching

5
ASAP ADS-33 Software Application Package
  • Will assist user in interpretation of
    requirements and compliance
  • MATLAB toolbox
  • Supported by Bob Heffley
  • Eventually plan to incorporate elements of
    Heffleys TPV (Task/Pilot/Vehicle) toolbox

6
Other Ongoing Research at HAI
  • FAA Rudder Study
  • Initial contract (write test plan) completed
  • Received additional funding for simulation study
    on NASA Ames VMS
  • Identify requirements for simulator motion
  • Four-week session in November
  • NASA Dryden Contract to Investigate Handling
    Qualities Criteria for Aircraft with Failed
    Surfaces
  • Extend interaxis coupling criteria from
    rotorcraft
  • Assess risk of pilot-induced oscillations
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