Accession Number:

AD0733181

Title:

Incorporation of the Six Dimensional, Linearized Equations of Motion with a Variable Stability Flight Simulator.

Descriptive Note:

Master's thesis,

Corporate Author:

NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF

Personal Author(s):

Report Date:

1971-09-01

Pagination or Media Count:

38.0

Abstract:

In this report the equations of motion for the six degrees of freedom of an aircraft were solved by an analog computer circuit. These solutions were incorporated with the instrumentation of a fixed base flight simulator to provide a variable stability aircraft demonstration device. Author

Subject Categories:

  • Test Facilities, Equipment and Methods

Distribution Statement:

APPROVED FOR PUBLIC RELEASE