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Effects of yaw and pitch motion on model attitude measurements

Author: Ping Tcheng; John S Tripp; Tom D Finley; Langley Research Center.; Langley Aeronautical Laboratory.
Publisher: Hampton, Va. : NASA, Langley Research Center, [1995]
Series: NASA technical memorandum, 4641.
Edition/Format:   Print book : National government publication : EnglishView all editions and formats
Database:WorldCat
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Additional Physical Format: Online version:
Tcheng, Ping.
Effects of yaw and pitch motion on model attitude measurements.
Hampton, Va. : NASA, Langley Research Center, [1995]
(OCoLC)755171770
Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: Ping Tcheng; John S Tripp; Tom D Finley; Langley Research Center.; Langley Aeronautical Laboratory.
OCLC Number: 45171383
Description: 8 pages
Series Title: NASA technical memorandum, 4641.
Responsibility: Ping Tcheng, John S. Tripp, and Tom D. Finley.

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