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Fidelity Assessment Of A Uh 60a Simulation On The Nasa Ames Vertical Motion Simulator
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723580147 Total Pages :324 pages Book Rating :4.5/5 (81 download)
Book Synopsis Fidelity Assessment of a Uh-60a Simulation on the NASA Ames Vertical Motion Simulator by : National Aeronautics and Space Administration (NASA)
Download or read book Fidelity Assessment of a Uh-60a Simulation on the NASA Ames Vertical Motion Simulator written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt: Helicopter handling qualities research requires that a ground-based simulation be a high-fidelity representation of the actual helicopter, especially over the frequency range of the investigation. This experiment was performed to assess the current capability to simulate the UH-60A Black Hawk helicopter on the Vertical Motion Simulator (VMS) at NASA Ames, to develop a methodology for assessing the fidelity of a simulation, and to find the causes for lack of fidelity. The approach used was to compare the simulation to the flight vehicle for a series of tasks performed in flight and in the simulator. The results show that subjective handling qualities ratings from flight to simulator overlap, and the mathematical model matches the UH-60A helicopter very well over the range of frequencies critical to handling qualities evaluation. Pilot comments, however, indicate a need for improvement in the perceptual fidelity of the simulation in the areas of motion and visual cuing. The methodology used to make the fidelity assessment proved useful in showing differences in pilot work load and strategy, but additional work is needed to refine objective methods for determining causes of lack of fidelity. Atencio, Adolph, Jr. Ames Research Center NASA-TM-104016, A-93071, NAS 1.15:104016, USAATC-TR-93-A-005, AD-A271172 RTOP 505-59-52...
Book Synopsis Fidelity Assessment of a UH-60A Simulation on the NASA Ames Vertical Motion Simulator by :
Download or read book Fidelity Assessment of a UH-60A Simulation on the NASA Ames Vertical Motion Simulator written by and published by . This book was released on 1993 with total page 326 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fidelity Assessment of a UH-60A Simulation on the NASA Ames Vertical Motion Simulator by :
Download or read book Fidelity Assessment of a UH-60A Simulation on the NASA Ames Vertical Motion Simulator written by and published by . This book was released on 1993 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on with total page 1168 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalogue, United States Public Documents by :
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Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1994 with total page 1716 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722090487 Total Pages :32 pages Book Rating :4.0/5 (94 download)
Book Synopsis Analysis Procedures and Subjective Flight Results of a Simulator Validation and Cue Fidelity Experiment by : National Aeronautics and Space Administration (NASA)
Download or read book Analysis Procedures and Subjective Flight Results of a Simulator Validation and Cue Fidelity Experiment written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-30 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: A joint experiment to investigate simulator validation and cue fidelity was conducted by the Dryden Flight Research Facility of NASA Ames Research Center (Ames-Dryden) and NASA Langley Research Center. The primary objective was to validate the use of a closed-loop pilot-vehicle mathematical model as an analytical tool for optimizing the tradeoff between simulator fidelity requirements and simulator cost. The validation process includes comparing model predictions with simulation and flight test results to evaluate various hypotheses for differences in motion and visual cues and information transfer. A group of five pilots flew air-to-air tracking maneuvers in the Langley differential maneuvering simulator and visual motion simulator and in an F-14 aircraft at Ames-Dryden. The simulators used motion and visual cueing devices including a g-seat, a helmet loader, wide field-of-view horizon, and a motion base platform. Carr, Peter C. and Mckissick, Burnell T. Ames Research Center RTOP 533-02-30...
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Book Synopsis Journal of the American Helicopter Society by : American Helicopter Society
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Book Synopsis NASA/FAA Helicopter Simulator Workshop by : William E. Larsen
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Book Synopsis Helicopter Simulation Validation Using Flight Data by : David L. Key
Download or read book Helicopter Simulation Validation Using Flight Data written by David L. Key and published by . This book was released on 1982 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The paper describes a joint NASA/Army effort to perform a systematic ground-based piloted simulation validation assessment. The best available mathematical model for the subject helicopter (UH-60A Black Hawk) was programmed for real-time operation. Flight data were obtained to validate the math model, and to develop models for the pilot control strategy while performing mission-type tasks. The validated mathe model will be combined with motion and visual systems to perform ground based simulation during April of 1983. Comparisons of the control strategy obtained in flight with that obtained on the simulator will be used as the basis for assessing the fidelity of the results obtained in the simulator. (Author).
