A Review and Comparison of Tactical Missile Control Methods

Abstract

Methods in use or proposed for the control of tactical missiles are identified, described, and compared. A brief and simplified discussion of missile response and flight dynamics is presented in order to illustrate the primary factors affecting control system performance. Aerodynamic (wing, tail, canard) controls are discussed as well as fluid interaction devices (thrust vector control, jet interaction, and others). Considering various performance factors, a rough comparison is made in an attempt to identify the most promising control methods for highly maneuverable missiles.

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Document Details

Document Type
Technical Report
Publication Date
Dec 20, 1972
Accession Number
AD0908213

Entities

People

  • Robert H. Nunn

Organizations

  • Naval Postgraduate School

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aerodynamic Forces
  • Aerodynamic Stability
  • Airframes
  • Boundary Layer
  • California
  • Control Surfaces
  • Control Systems
  • Control Systems Engineering
  • Flight Paths
  • Fluid Control
  • Fluid Dynamics
  • Guided Missiles
  • Mach Number
  • Movable Nozzles
  • Navy
  • Pressure Distribution
  • Rocket Engines
  • Test And Evaluation
  • United States

Readers

  • Aerodynamics/Aeronautics.
  • Systems Analysis and Design