AN ANALYTICAL INVESTIGATION OF FLIGHT CONTROL PROBLEMS AND STATIC AND DYNAMIC RESPONSE REQUIREMENTS OF A HIGH-SPEED, LOW-ALTITUTE MISSILE

Abstract

The results of a study of the flight control problems of a high-speed, low-altitude missile are presented. Investigations were also made in the areas of gust analysis; reactor, inlet, and control system coupling; and basic vehicle stability and control. The effects of sampling frequency (data rate), computation time delay, and transport lags on over-all system performance are presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1961
Accession Number
AD0269253

Entities

People

  • J.f.l. Lee
  • R.c.k. Lee

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Computations
  • Control Systems
  • Couplings
  • Data Rate
  • Dynamic Response
  • Elevation
  • Frequency
  • Low Altitude
  • Sampling
  • Transport Ships
  • Vehicles

Readers

  • Aerospace Engineering
  • Control Systems Engineering.