Qualitative Simulator Study of Longitudinal Stick Forces and Displacements Desirable During Tracking PDF Download
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Author: Stanley Faber
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 680
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Book Description
In this study in which an airplane simulator with one degree of freedom (pitch) was used, results were determined for three conditions of airplane dynamics. For an undamped natural frequency of 1/2 cps with a damping ratio of 0.18 and for an undamped natural frequency of 1 cps with a damping ratio of 0.11, moderate longitudinal stick forces and displacements were desired.
Author: Stanley Faber
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 680
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Book Description
In this study in which an airplane simulator with one degree of freedom (pitch) was used, results were determined for three conditions of airplane dynamics. For an undamped natural frequency of 1/2 cps with a damping ratio of 0.18 and for an undamped natural frequency of 1 cps with a damping ratio of 0.11, moderate longitudinal stick forces and displacements were desired.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1274
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Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 770
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1698
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 382
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Book Description
Author: J. C. Gibson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 180
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Book Description
Since the earliest days of manned flight, designers have to sought to assist the pilot in the performance of tasks by using stick and feel systems to bring these tasks within the bounds of human physical capabilities. This volume describes stick and feel systems in two parts. Part one describes the technologies which have been developed throughout the history of 20th Century aviation. Part two describes how modern systems dynamics interact with the human pilot. It is hoped that the design lessons and approaches outlined in this volume will contribute to a better understanding and appreciation of the importance of force-feel system design in aircraft/rotorcraft flight control.
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Human engineering
Languages : en
Pages : 198
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Book Description
Author: Irving L. Ashkenas
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 96
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Book Description
