000021280 001__ 21280
000021280 005__ 20170522124347.0
000021280 04107 $$aeng
000021280 046__ $$k2017-05-15
000021280 100__ $$aĆwiklak, J.
000021280 24500 $$aDESIGNATION THE VELOCITY OF CESSNA 172 AIRCRAFT BASED ON GPS DATA IN FLIGHT TEST

000021280 24630 $$n23.$$pEngineering Mechanics 2017
000021280 260__ $$bBrno University of Technology, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno
000021280 506__ $$arestricted
000021280 520__ $$2eng$$aIn recent years the GPS satellite receiver is a basic equipment of avionics onboard of aircraft. Especially, the GPS receiver is utilized for designation the component of PV (Position-Velocity) model of the aircraft in kinematic mode in air navigation. The mathematical scheme of recovery the velocity of aircraft in local frame ENU (East-North-Up) is presented in this article. As part of research works a values of velocity of motion of the aircraft were appointed and showed.

000021280 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000021280 653__ $$aGPS, Velocity, ENU frame, Aircraft.

000021280 7112_ $$aEngineering Mechanics 2017$$cSvratka, CZ$$d2017-05-15 / 2017-05-18$$gEM2017
000021280 720__ $$aĆwiklak, J.$$iJafernik, H.$$iKrasuski, K.
000021280 8560_ $$ffischerc@itam.cas.cz
000021280 8564_ $$s757033$$uhttps://invenio.itam.cas.cz/record/21280/files/0262.pdf$$yOriginal version of the author's contribution in proceedings, page 262, section KIN.
000021280 962__ $$r21225
000021280 980__ $$aPAPER