Linearized mathematical models for De Havilland Canada

MacDonald, R. A.; Garelick, Mel; O'Grady, J.; John A. Volpe National Transportation Systems Center (U.S.)

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

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

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English

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Creators:

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

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

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

[+]

Aerodynamic Lift Air Traffic Control Drag Mathematical Models Stability (Mechanics) STOL Aircraft
Publication/ Report Number:

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

Tech Report
Corporate Publisher:

United States. 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.
Format:

PDF
Collection(s):

Volpe Center
Main Document Checksum:

[+]

urn:sha256:c0379daa5a89d76c96e0705e279a6b4a242ffcbd43da95242a0858b517f2cfca
Download URL:

https://rosap.ntl.bts.gov/view/dot/9168/dot_9168_DS1.pdf
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Linearized mathematical models for De Havilland Canada "Buffalo & Twin Otter" STOL transports.

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