Dynamics Report for T-28B Simplified Flight Simulator.

Abstract

A study was conducted to develop a method and approach by which specific characteristics of the NAA T-28B aircraft are to be simulated. This includes also the aerodynamic design data developed and needed for computer programming; aircraft equations of motion and position; simulator equations of motion and position; simulator instrument, aircraft systems, flight control and engine equations; definition of symbols, subscripts, and mathematical notation; aerodynamic coefficients and their data source; cockpit layout; and control feel design. The mathematical models for the T-28B aircraft developed under this study are applicable at a fixed gross weight of 7700 lbs and 25% c.g. location. A simplified solution for the throttle movement versus thrust horsepower output relationship was also developed. (Modified author abstract)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1973
Accession Number
AD0774479

Entities

People

  • Moses Aronson

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Computer Programming
  • Computers
  • Equations
  • Equations Of Motion
  • Flight Simulators
  • Mathematical Models
  • Simulators

Readers

  • Aerospace Engineering
  • Aviation Science / Aeronautics.
  • Control Systems Engineering.