DIGITAL COMPUTER SIMULATION OF THE X-22A, SIX DEGREES OF FREEDOM EQUATIONS OF MOTION AND GLOBAL AERODYNAMICS,

Abstract

The equations of motions for analyzing dynamics, stability and control of a VTOL aircraft (X-22A) have been programmed for solution on the IBM 360/65. Included in this report are a description of the general characteristics of the problem, the mathematical statement of the problem and instructions in the use of this program. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 25, 1968
Accession Number
AD0830494

Entities

People

  • Clarence Mesiah

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamics
  • Aircrafts
  • Computational Science
  • Computer Simulations
  • Computers
  • Computing-Related Activities
  • Control Simulators
  • Digital Computers
  • Dynamics
  • Equation-Based Simulations
  • Equations
  • Equations Of Motion
  • Instructions
  • Simulations
  • Simulators

Fields of Study

  • Mathematics
  • Physics

Readers

  • Aerospace Engineering
  • Computer Science.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)