000012409 001__ 12409
000012409 005__ 20160816141443.0
000012409 04107 $$aeng
000012409 046__ $$k2016-05-09
000012409 100__ $$aGrzyb, M.
000012409 24500 $$aTHE USE OF SPECIAL ALGORITHM TO CONTROL THE FLIGHT OF ANTI-AIRCRAFT MISSILE

000012409 24630 $$n22.$$pEngineering Mechanics 2016
000012409 260__ $$bInstitute of Thermomechanics AS CR, v.v.i., Praha
000012409 506__ $$arestricted
000012409 520__ $$2eng$$aThe paper analyzes a possibility of using the special algorithm to control the flight of a homing air target missile. The method is based on the signum function and utilizes the phase trajectories of errors resulting from the adopted homing method (proportional navigation). The results obtained via Matlab package are presented in graphical form.

000012409 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000012409 653__ $$adynamics, phase trajectories, homing, missile, control.

000012409 7112_ $$aEngineering Mechanics 2016$$cSvratka, CZ$$d2016-05-09 / 2016-05-12$$gEM2016
000012409 720__ $$aGrzyb, M.$$iStefanski, K.
000012409 8560_ $$ffischerc@itam.cas.cz
000012409 8564_ $$s418352$$uhttps://invenio.itam.cas.cz/record/12409/files/039bo_p_dyn.pdf$$yOriginal version of the author's contribution as presented on CD, id 039, section DYN.
000012409 962__ $$r12369
000012409 980__ $$aPAPER