X 22a Fixed Base Ground Simulator Facility
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Author | : T. J. Gavin |
Publisher | : |
Total Pages | : 42 |
Release | : 1973 |
Genre | : |
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Download X-22A Fixed-Base Ground Simulator Facility Book in PDF, Epub and Kindle
The report presents a description of the X-22A fixed-base ground simulator facility. The simulation will be used in conjunction with the X-22A V/STOL aircraft which is a unique research tool used in performing flying qualities research. The simulator duplicates the X-22A aircraft and its systems for varying pertinent pitch, roll, yaw and thrust stability derivatives. A high-speed process control digital computer is used to solve the X-22A equations of motion including the nonlinear characteristics associated with transition, and provides the signals for the displays and variable stability system. The X-22A ground simulator is a facility that consists of an air conditioned flight simulation cockpit and a mobile van. (Modified author abstract).
Author | : |
Publisher | : |
Total Pages | : 688 |
Release | : 1983 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, Epub and Kindle
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author | : Jerome L. Michaels |
Publisher | : |
Total Pages | : 132 |
Release | : 1969 |
Genre | : |
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Download Study and Evaluation of V/Stol Ground-Based Simulation Techniques for the X-22A Aircraft Book in PDF, Epub and Kindle
Three types of ground-based simulators of the X-22A aircraft are evaluated and compared with actual flight. Simulator types employed were a fixed-base simulator with linearized equations of motion, a fixed-base simulator with nonlinearized equations of motion, and a moving-base simulator with linearized equations of motion. Evaluations are based on comparisons of pilot ratings, pilot comments, and dynamic response time history data. Data comparisons are interpreted and discussed in terms of significant factors such as simulator type, complexity, and physical and psychological cues. Several correlations among the different simulators and flight are developed in terms of numerical pilot ratings of specific flight conditions and tasks. These pilot rating correlations provide a basis for projecting flight characteristics from results obtained with the simulator types evaluated. Relative capabilities and limitations of the various simulators to represent flight and minimum standards of adequacy for specific tasks are also established for hover and transition. (Author).
Author | : |
Publisher | : |
Total Pages | : 1000 |
Release | : 1974 |
Genre | : Research |
ISBN | : |
Download Government Reports Announcements Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1108 |
Release | : 1979 |
Genre | : Science |
ISBN | : |
Download Government Reports Announcements & Index Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 548 |
Release | : 1974 |
Genre | : Aeronautics |
ISBN | : |
Download Aeronautical Engineering Book in PDF, Epub and Kindle
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Author | : |
Publisher | : |
Total Pages | : 1074 |
Release | : 1975 |
Genre | : Government publications |
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Download Government Reports Index Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 942 |
Release | : 1979 |
Genre | : Government reports announcements & index |
ISBN | : |
Download Government Reports Annual Index Book in PDF, Epub and Kindle
Author | : Edwin W. Aiken |
Publisher | : |
Total Pages | : 97 |
Release | : 1974 |
Genre | : |
ISBN | : |
Download A Fixed-Base Ground Simulator Study of Control and Display Requirements for VTOL Instrument Landings with a Decelerating Approach to a Hover Book in PDF, Epub and Kindle
An exploratory study of the control and display requirements for performing decelerating transition landings on instruments with the X-22A aircraft was conducted utilizing the X-22A fixed-base ground simulator as a test bed. This experiment was prerequisite for an in-flight VTOL Transition Landing Program using the variable stability X-22A as a research vehicle. Both full and partial transitions to a hover were flown along a 10 degrees glide path at deceleration levels of up to 0.1 g. Various control/display system combinations were designed, developed, and evaluated for the task. Two specific objectives of the experiment were to investigate the benefits of a direct velocity control system, as opposed to the normal X-22A thrust controls, and to determine the feasibility of adapting, through electronic rather than mechanical means, the X-22A duct rotation system to direct velocity control. (Modified author abstract).
Author | : |
Publisher | : |
Total Pages | : 1392 |
Release | : 1974 |
Genre | : Technology |
ISBN | : |
Download Government Reports Announcements Book in PDF, Epub and Kindle