"12112_12_1" . "124884" . "\u0160torch, V\u00EDt" . "Filipsk\u00FD, Jakub" . "Bezpilotn\u00ED l\u00E9taj\u00EDc\u00ED aerodynamick\u00E1 zku\u0161ebna"@cs . . "RIV/68407700:21220/12:00204119" . . . "4"^^ . . "http://fluids.fs.cvut.cz/www/" . . "Unmanned flying aerodynamic test bed"@en . . "[A9A063622786]" . "RIV/68407700:21220/12:00204119!RIV13-MSM-21220___" . . "Unmanned flying aerodynamic test bed"@en . "4"^^ . "Bezpilotn\u00ED l\u00E9taj\u00EDc\u00ED aerodynamick\u00E1 zku\u0161ebna" . . . "21220" . "The airplane of classical design and maximum takeoff weight 20Kg is powered by electric motor in combination with lithium accumulators. The design is adapted to the materials and technology used and the purpose of the craft. The airframe is mostly made of balsa wood and ply with composite parts. In order to measure the aerodynamic properties of airfoils the airplane is equipped with removable end sections of the wing with the measured airfoil and static pressure probes. The static pressure is measured and recorded by a sensor board developed at the department. Current position, orientation, speed and other flight data are recorded during flight. The flight can be controlled either from the ground with automatic stabilization enabled or fully automatic along preprogrammed route."@en . "\u010C\u00ED\u017Eek, Jan" . . "Bezpilotn\u00ED l\u00E9taj\u00EDc\u00ED aerodynamick\u00E1 zku\u0161ebna"@cs . . . . . . . "aerodynamic test bed; in flight measurement; airfoil; autonomous flight; pressure distribution; flight data recording"@en . "p\u0159ibli\u017En\u00E9 n\u00E1klady na materi\u00E1l 34 000,-" . . "rozp\u011Bt\u00ED nastaviteln\u00E9 3,4-4,4m, hmotnost 20kg, rychlost letu 20m/s" . . . . "Letoun klasick\u00E9 koncepce o vzletov\u00E9 hmotnosti do 20kg je poh\u00E1n\u011Bn elektromotorem v kombinaci s lithiov\u00FDmi akumul\u00E1tory. Konstrukce je p\u0159izp\u016Fsobena pou\u017Eit\u00E9 technologii stavby, materi\u00E1lu a \u00FA\u010Delu. Drak letounu je p\u0159ev\u00E1\u017En\u011B z balzov\u00E9ho d\u0159eva a leteck\u00E9 p\u0159ekli\u017Eky, vyztu\u017Een\u00FD a dopln\u011Bn\u00FD kompozitov\u00FDmi prvky. Za \u00FA\u010Delem m\u011B\u0159en\u00ED parametr\u016F leteck\u00FDch profil\u016F je letoun vybaven sn\u00EDmateln\u00FDmi koncov\u00FDmi \u00FAseky k\u0159\u00EDdel s po\u017Eadovan\u00FDm profilem a odb\u011Bry statick\u00E9ho tlaku. Statick\u00FD tlak je vyhodnocov\u00E1n citlivou m\u011B\u0159ic\u00ED technikou vyvinutou na \u00FAstavu. B\u011Bhem letu je zaznamen\u00E1v\u00E1na okam\u017Eit\u00E1 poloha a orientace letounu v prostoru, rychlost a dal\u0161\u00ED letov\u00E9 \u00FAdaje. Let m\u016F\u017Ee b\u00FDt \u0159\u00EDzen ze zem\u011B, kdy je letoun automaticky stabilizov\u00E1n, nebo pln\u011B automaticky, kdy letoun sleduje nastavenou trasu." . . "I" . . . . "No\u017Ei\u010Dka, Ji\u0159\u00ED" . . "Letoun klasick\u00E9 koncepce o vzletov\u00E9 hmotnosti do 20kg je poh\u00E1n\u011Bn elektromotorem v kombinaci s lithiov\u00FDmi akumul\u00E1tory. Konstrukce je p\u0159izp\u016Fsobena pou\u017Eit\u00E9 technologii stavby, materi\u00E1lu a \u00FA\u010Delu. Drak letounu je p\u0159ev\u00E1\u017En\u011B z balzov\u00E9ho d\u0159eva a leteck\u00E9 p\u0159ekli\u017Eky, vyztu\u017Een\u00FD a dopln\u011Bn\u00FD kompozitov\u00FDmi prvky. Za \u00FA\u010Delem m\u011B\u0159en\u00ED parametr\u016F leteck\u00FDch profil\u016F je letoun vybaven sn\u00EDmateln\u00FDmi koncov\u00FDmi \u00FAseky k\u0159\u00EDdel s po\u017Eadovan\u00FDm profilem a odb\u011Bry statick\u00E9ho tlaku. Statick\u00FD tlak je vyhodnocov\u00E1n citlivou m\u011B\u0159ic\u00ED technikou vyvinutou na \u00FAstavu. B\u011Bhem letu je zaznamen\u00E1v\u00E1na okam\u017Eit\u00E1 poloha a orientace letounu v prostoru, rychlost a dal\u0161\u00ED letov\u00E9 \u00FAdaje. Let m\u016F\u017Ee b\u00FDt \u0159\u00EDzen ze zem\u011B, kdy je letoun automaticky stabilizov\u00E1n, nebo pln\u011B automaticky, kdy letoun sleduje nastavenou trasu."@cs . "Bezpilotn\u00ED l\u00E9taj\u00EDc\u00ED aerodynamick\u00E1 zku\u0161ebna" .