Analytical Study of the Performance of a Gust Alleviation System with a Vane Sensor
Author: Waldo I. Oehman
Publisher:
Published: 1974
Total Pages: 36
ISBN-13:
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Author: Waldo I. Oehman
Publisher:
Published: 1974
Total Pages: 36
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DOWNLOAD EBOOKAuthor: Masaki Komoda
Publisher:
Published: 1976
Total Pages: 68
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DOWNLOAD EBOOKAuthor: United States. Congress. House. Committee on Science and Astronautics. Subcommittee on Aeronautics and Space Technology
Publisher:
Published: 1974
Total Pages: 344
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Published: 1995
Total Pages: 488
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DOWNLOAD EBOOKLists 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: United States. Congress. House. Science and Astronautics Committee
Publisher:
Published: 1974
Total Pages: 340
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DOWNLOAD EBOOKAuthor: United States. Congress. House. Committee on Science and Astronautics
Publisher:
Published: 1974
Total Pages: 1456
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DOWNLOAD EBOOKAuthor: United States. Congress. House. Committee on Science and Astronautics. Subcommittee on International Cooperation in Science and Space
Publisher:
Published: 1974
Total Pages: 2304
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Published: 1971
Total Pages: 1508
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DOWNLOAD EBOOKAuthor: Terry A. Hammond
Publisher:
Published: 1984
Total Pages: 372
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DOWNLOAD EBOOKThis project was initiated based on the goal of making the ride of the commuter aircraft as smooth as the ride experienced on the major commercial airliners. The objectives of this project were to design a digital, longitudinal mode ride quality augmentation system (RQAS) for a commuter aircraft, and to investigate the effect of selected parameters on those designs. The initial stage of this research was the development of an interactive control augmentation design (ICAD) program for use in the design and evaluation of the candidate RQASs. This computer aided design program included both optimal and classical design approaches for either continuous or digital systems, and provided data for analyses in both the time and frequency domains. Both optimal and classical RQAS designs were generated for the five flight conditions selected as representative of a typical commuter mission, using a Cessna 402B. These RQASs used direct lift flaps and the elevator for control of the longitudinal accelerations. The design parameters selected include the sample time, computation delay time, servo bandwidth, and the flap and elevator control power. Optimal and classical point designs, based on the nominal design parameters, are presented for all five flight conditions. Parametric analyses for all five flight condition for both the optimal and classical designs are also presented.