Linearized mathematical models for De Havilland Canada "Buffalo & Twin Otter" STOL transports.

MacDonald, R. A.; Garelick, Mel; O'Grady, J.

i

Linearized mathematical models for De Havilland Canada "Buffalo & Twin Otter" STOL transports.

1971-06-01
By MacDonald, R. A. ; Garelick, Mel ; O'Grady, J.

File Language:

English

Details

Creators:

MacDonald, R. A. ; Garelick, Mel ; O'Grady, J.
Corporate Creators:

John A. Volpe National Transportation Systems Center (U.S.)
Subject/TRT Terms:
Publication/ Report Number:

DOT-TSC-FAA-71-8
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration
Abstract:

Linearized six degree of freedom rigid body aircraft equations of motion are presented in a stability axes system. Values of stability derivatives are estimated for two representative STOL aircraft - the DeHavilland of Canada 'Buffalo' and 'Twin Otter.' These estimates are based on analytical expressions included in the report. The combination of the equations of motion and the estimated stability derivatives provides an aircraft model which is useful for Navigation, Guidance and ATC Studies. Resulting transient responses to control inputs are presented.
Content Notes:

112p. in various pagings
Format:

PDF
Download URL:

https://rosap.ntl.bts.gov/view/dot/9168/dot_9168_DS1.pdf
File Type:

[PDF - 5.41 MB]
Collection(s):

Volpe Center
Main Document Checksum:

urn:sha-512:3e0c52f079f29ae2543cc1faecdee0201218be1d4e862b39a857ce122a6ca209537bc48fb4a875a8abbe47a33a7f425651acb8ed8420404bd0ab8666a2546775

File Language:

English

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