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

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)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1971
Accession Number
AD0733181

Entities

People

  • Merlin Richard Heckemeyer

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Analog Computers
  • Computers
  • Control Simulators
  • Demonstrations
  • Equations
  • Equations Of Motion
  • Flight Simulators
  • Instrumentation
  • Simulations
  • Simulators
  • Variable Stability Aircraft

Readers

  • Aviation Science / Aeronautics.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)