Accession Number:

ADP011105

Title:

Impulse Control of Anti-Tank Mortar Missile

Descriptive Note:

Corporate Author:

WARSAW UNIV POLAND

Personal Author(s):

Report Date:

2001-06-01

Pagination or Media Count:

8.0

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.

Subject Categories:

  • Guided Missiles
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE