Proposed Yaw-Axis Target Acquisition and Tracking Handling Qualities Requirement Updates.

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Title: Proposed Yaw-Axis Target Acquisition and Tracking Handling Qualities Requirement Updates.
Authors: Berger, Tom1 tom.berger2.civ@army.mil, Gong, Anthony1, Lusardi, Jeffery A.1, Mansur, M. Hossein1, Boehringer, Ryan P.2, Ogden, Wesley R.2, Ott, Carl R.2, Brown, Daniel R.3, Daniels, David A.3, Borden, Christopher C.4
Source: Journal of the American Helicopter Society. Oct2025, Vol. 70 Issue 4, p042005-1-042005-16. 16p.
Subjects: Target acquisition, Automatic tracking, Bandwidths, Rotorcraft, Pilot projects
Abstract: A piloted simulation experiment was conducted in the NASA Ames Vertical Motion Simulator to investigate the effects of bandwidth, phase delay, attitude quickness, and maximum achievable rate on yaw-axis handling qualities in hover and forward flight. Two different aircraft were tested, representative of advanced scout-class rotorcraft. Five target acquisition and tracking mission task elements were used in the study. Two of the tasks were modified versions of tasks used to determine the ADS-33E target acquisition and tracking yaw attitude quickness boundaries. Two of the tasks were modified versions of attitude capture and hold and sum-of-sines tracking tasks previously used to evaluate pitch and roll axis handling qualities. The final task was a forward flight target acquisition task developed for this study based on a ground attack or strafing maneuver. Eight Army pilots participated in the study and evaluated 60 yaw-axis configurations. The results of the study suggest that the current yaw-axis hover/low-speed and forward flight bandwidth and hover/low-speed attitude quickness requirements for target acquisition and tracking are too low. Updated boundaries for these requirements are recommended. [ABSTRACT FROM AUTHOR]
Copyright of Journal of the American Helicopter Society is the property of American Helicopter Society dba Vertical Flight Society and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
Database: Engineering Source
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  Data: Proposed Yaw-Axis Target Acquisition and Tracking Handling Qualities Requirement Updates.
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  Data: <searchLink fieldCode="AR" term="%22Berger%2C+Tom%22">Berger, Tom</searchLink><relatesTo>1</relatesTo><i> tom.berger2.civ@army.mil</i><br /><searchLink fieldCode="AR" term="%22Gong%2C+Anthony%22">Gong, Anthony</searchLink><relatesTo>1</relatesTo><br /><searchLink fieldCode="AR" term="%22Lusardi%2C+Jeffery+A%2E%22">Lusardi, Jeffery A.</searchLink><relatesTo>1</relatesTo><br /><searchLink fieldCode="AR" term="%22Mansur%2C+M%2E+Hossein%22">Mansur, M. Hossein</searchLink><relatesTo>1</relatesTo><br /><searchLink fieldCode="AR" term="%22Boehringer%2C+Ryan+P%2E%22">Boehringer, Ryan P.</searchLink><relatesTo>2</relatesTo><br /><searchLink fieldCode="AR" term="%22Ogden%2C+Wesley+R%2E%22">Ogden, Wesley R.</searchLink><relatesTo>2</relatesTo><br /><searchLink fieldCode="AR" term="%22Ott%2C+Carl+R%2E%22">Ott, Carl R.</searchLink><relatesTo>2</relatesTo><br /><searchLink fieldCode="AR" term="%22Brown%2C+Daniel+R%2E%22">Brown, Daniel R.</searchLink><relatesTo>3</relatesTo><br /><searchLink fieldCode="AR" term="%22Daniels%2C+David+A%2E%22">Daniels, David A.</searchLink><relatesTo>3</relatesTo><br /><searchLink fieldCode="AR" term="%22Borden%2C+Christopher+C%2E%22">Borden, Christopher C.</searchLink><relatesTo>4</relatesTo>
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  Data: <searchLink fieldCode="JN" term="%22Journal+of+the+American+Helicopter+Society%22">Journal of the American Helicopter Society</searchLink>. Oct2025, Vol. 70 Issue 4, p042005-1-042005-16. 16p.
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  Data: <searchLink fieldCode="DE" term="%22Target+acquisition%22">Target acquisition</searchLink><br /><searchLink fieldCode="DE" term="%22Automatic+tracking%22">Automatic tracking</searchLink><br /><searchLink fieldCode="DE" term="%22Bandwidths%22">Bandwidths</searchLink><br /><searchLink fieldCode="DE" term="%22Rotorcraft%22">Rotorcraft</searchLink><br /><searchLink fieldCode="DE" term="%22Pilot+projects%22">Pilot projects</searchLink>
– Name: Abstract
  Label: Abstract
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  Data: A piloted simulation experiment was conducted in the NASA Ames Vertical Motion Simulator to investigate the effects of bandwidth, phase delay, attitude quickness, and maximum achievable rate on yaw-axis handling qualities in hover and forward flight. Two different aircraft were tested, representative of advanced scout-class rotorcraft. Five target acquisition and tracking mission task elements were used in the study. Two of the tasks were modified versions of tasks used to determine the ADS-33E target acquisition and tracking yaw attitude quickness boundaries. Two of the tasks were modified versions of attitude capture and hold and sum-of-sines tracking tasks previously used to evaluate pitch and roll axis handling qualities. The final task was a forward flight target acquisition task developed for this study based on a ground attack or strafing maneuver. Eight Army pilots participated in the study and evaluated 60 yaw-axis configurations. The results of the study suggest that the current yaw-axis hover/low-speed and forward flight bandwidth and hover/low-speed attitude quickness requirements for target acquisition and tracking are too low. Updated boundaries for these requirements are recommended. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
  Label:
  Group: Ab
  Data: <i>Copyright of Journal of the American Helicopter Society is the property of American Helicopter Society dba Vertical Flight Society and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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        Value: 10.4050/JAHS.70.042005
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      – Code: eng
        Text: English
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        PageCount: 16
        StartPage: 042005-1
    Subjects:
      – SubjectFull: Target acquisition
        Type: general
      – SubjectFull: Automatic tracking
        Type: general
      – SubjectFull: Bandwidths
        Type: general
      – SubjectFull: Rotorcraft
        Type: general
      – SubjectFull: Pilot projects
        Type: general
    Titles:
      – TitleFull: Proposed Yaw-Axis Target Acquisition and Tracking Handling Qualities Requirement Updates.
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            – D: 01
              M: 10
              Text: Oct2025
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              Y: 2025
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