Impulse Control of Anti-Tank Mortar Missile

Abstract

Report explains problem of control dynamics of flying object with discontinuous impulse control inputs. Control is realised by the rocket correction motors locate around the centre of gravity of flying object. Start up the motor causes formation the force impulse direct perpendicular to main symmetry axis of object and direct along axis crossing object gravity centre. We tested possibilities of more effective influence on speed vector by impulse correction motors.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2001
Accession Number
ADP011105

Entities

People

  • Robert Glebocki
  • Ryszard Vogt

Organizations

  • University of Warsaw

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Applied Mechanics
  • Center Of Gravity
  • Computer Simulations
  • Control Systems
  • Differential Equations
  • Errors
  • Gravity
  • Guidance
  • Impact Point
  • Mechanics
  • Military Aircraft
  • Projectiles
  • Proportional Navigation
  • Rocket Engines
  • Rockets
  • Vehicles

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Electrical Engineering
  • Sensor Fusion and Tracking Systems.