000021347 001__ 21347
000021347 005__ 20170522124350.0
000021347 04107 $$aeng
000021347 046__ $$k2017-05-15
000021347 100__ $$aKrzysztofik, I.
000021347 24500 $$aAPPLICATION OF THE SLIDING CONTROLLER FOR THE GYROSCOPE SYSTEM OF THE ANTI-AIRCRAFT MISSILE

000021347 24630 $$n23.$$pEngineering Mechanics 2017
000021347 260__ $$bBrno University of Technology, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno
000021347 506__ $$arestricted
000021347 520__ $$2eng$$aPrecision of anti-aircraft missile homing depends mainly on correct determination of the current angle between the axis of the gyroscope system and the line of sight. The system of automatic gyroscope control should ensure automatic minimization of that angle, and thus, constant directing of the gyroscope system axis towards the line of sight, i.e. tracking the target by the homing head. This paper presents a sliding controller applied to control the gyroscope system. Subsequently, the dynamics of that system during the process of anti-aircraft missile homing onto a moveable target was studied. Some chosen results of the simulation research were presented graphically.

000021347 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000021347 653__ $$aGyroscope system, Sliding controller, Missile.

000021347 7112_ $$aEngineering Mechanics 2017$$cSvratka, CZ$$d2017-05-15 / 2017-05-18$$gEM2017
000021347 720__ $$aKrzysztofik, I.$$iKoruba, Z.
000021347 8560_ $$ffischerc@itam.cas.cz
000021347 8564_ $$s948997$$uhttps://invenio.itam.cas.cz/record/21347/files/0530.pdf$$yOriginal version of the author's contribution in proceedings, page 530, section DYN.
000021347 962__ $$r21225
000021347 980__ $$aPAPER