Impulse Control of Anti-Tank Mortar Missile
WARSAW UNIV POLAND
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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.
- Guided Missiles
- Rocket Engines