Accession Number:

AD0860071

Title:

An Analog Simulation of Aircraft Stability and Control Using Non-Linear Equations of Motion.

Personal Author(s):

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING

Report Date:

1969-06-01

Abstract:

A study was made to determine the feasibility of programing an analog simulation of aircraft stability on a general-purpose analog computer using non-linear differential equations. The simulation was to demonstrate the effects of inertial cross-coupling. An F-4 aircraft was simulated at two different reference flight conditions using the equations derived in the study. Author

Descriptive Note:

Master's Thesis,

Pages:

0087

Descriptors:

Identifiers:

Subject Categories:

Communities Of Interest:

File Size:

0.00MB

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