HIGH-PRECISION SELF-OSCILLATING ATTITUDE CONTROL FOR SMALL-SIZED CONTROLLABLE PROJECTILES

摘要

FIELD: aeronautical engineering. ^ SUBSTANCE: proposed attitude control includes power supply source, DC amplifier, summing-up unit and servo unit with control electromagnet connected with control surfaces. Provision is also made for correcting filter whose input is connected with summing-up unit and output is connected with DC amplifier. ^ EFFECT: enhanced accuracy. ^ 3 dwg