Guidance and Control Technology

Abstract

The fundamental ideas and the basic mathematics of the most common missile guidance laws are outlined. Rules of thumb for the required lateral acceleration for the different guidance laws are given. A brief summary of flight mechanics is given. The pitch axis control is treated and the dynamic properties are identified. Design of the autopilot for the inner loop using modem methods of controller design is briefly outlined.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2001
Accession Number
ADP010953

Entities

People

  • Erik Berglund

Organizations

  • Swedish Defence Research Agency

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Algorithms
  • Control Systems
  • Coordinate Systems
  • Equations
  • Equations Of Motion
  • Flight Control Systems
  • Guidance
  • Guided Bombs
  • Guided Missiles
  • Guided Weapons
  • Line Of Sight
  • Measurement
  • Navigation
  • Proportional Navigation
  • Trajectories
  • Weapon Control
  • Weapons

Readers

  • Control Systems Engineering.
  • Systems Analysis and Design