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Rotorcraft Flight Dynamics and Controls Research at NASAIn recent years, NASA has invested in key activities in the areas of flight controls, handling qualities and operations of rotorcraft for civilian applications. More specifically, the flight dynamics and control discipline has focused on analyzing the unique flight control and handling qualities challenges of large rotary wing vehicles anticipated for future passenger service, and examining the effect of control system augmentation on handling qualities for current civilian helicopters in order to improve safety and reduce accident rates. This paper highlights two recent research efforts in these areas. The first is an examination of flight control and handling qualities aspects of large rotorcraft. A series of experiments were performed in the large-motion Vertical Motion Simulator at NASA Ames Research Center to quantify the effects of vehicle size on flight control requirements and piloted handling qualities. These experiments used a large tilt-rotor concept (~100 passengers) to also investigate the control augmentation required to obtain Level 1 handling qualities for a vehicle of this size. The second is an examination of the effect of control system augmentation on handling qualities for current civil rotorcraft, like those currently used for Emergency Medical Service type operations. Many current civilian helicopters have rate response type control systems and little or no control system augmentation, although current technologies allow helicopters to be fitted with stability augmentation systems, either as standard equipment or aftermarket options. A simulation experiment was conducted in the Vertical Motion Simulator to quantify the effects of advanced control modes available with a partial authority stability augmentation system on task performance and handling qualities in both good and degraded visual conditions. In addition to providing an overview of the rotary wing flight dynamics and controls research at NASA, this paper will provide an overview of these two research activities along with key results and conclusions.
Document ID
20190027087
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Theodore, Colin R.
(NASA Ames Research Center Moffett Field, CA, United States)
Malpica, Carlos A.
(NASA Ames Research Center Moffett Field, CA, United States)
Lawrence, Ben
(San Jose State Univ. Moffett Field, CA, United States)
Date Acquired
July 9, 2019
Publication Date
December 18, 2014
Subject Category
Research And Support Facilities (Air)
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN17816
Report Number: ARC-E-DAA-TN17816
Meeting Information
Meeting: Australian Pacific Vertiflite Conference on Helicopter Technology
Location: Melbourne
Country: Australia
Start Date: December 18, 2014
End Date: December 19, 2014
Sponsors: Vertical Flight Society
Funding Number(s)
CONTRACT_GRANT: NNX12AB08A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Rotorcraft
Controls Research
Flight Dynamics
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