. "Za\u0159\u00EDzen\u00ED poskytuje koeficient deltaP/Pc, bu\u010F p\u0159esn\u011Bj\u0161\u00ED metodou (p\u0159ednost 0.5\u00B0), nebo klasicky (p\u0159ednost 1\u00B0)." . . . . "RIV/68407700:21230/11:00180531" . . "Pa\u010Des, Pavel" . . . . "AOAaAOSaSPEED" . . . . "RIV/68407700:21230/11:00180531!RIV12-TA0-21230___" . . "21230" . . . . . "Modul m\u011B\u0159en\u00ED rychlosti letu, \u00FAhlu n\u00E1b\u011Bhu a \u00FAhlu vybo\u010Den\u00ED"@cs . . "An Air-speed, Angle-of-attack and Angle-of-sideslip Measurement Module"@en . "\u0160ipo\u0161, Martin" . . . "Modul m\u011B\u0159en\u00ED rychlosti letu, \u00FAhlu n\u00E1b\u011Bhu a \u00FAhlu vybo\u010Den\u00ED" . "213371" . . "\u00FAhel n\u00E1b\u011Bhu; \u00FAhel vybo\u010Den\u00ED; rychlost; AOA; AOS; Air speed; ratio deltaP/Pc"@en . "Hospod\u00E1\u0159, Pavel" . "Popelka, Jan" . "Laborato\u0159 s151" . "P(GD102/09/H082), P(TA01030651), S, Z(MSM6840770015)" . "Levora, Tom\u00E1\u0161" . "Modul m\u011B\u0159en\u00ED rychlosti letu, \u00FAhlu n\u00E1b\u011Bhu a \u00FAhlu vybo\u010Den\u00ED"@cs . "AOAaAOSaSPEED je funk\u010Dn\u00ED vzorek, kter\u00FD umo\u017E\u0148uje za pou\u017Eit\u00ED MEMS senzor\u016F tlaku m\u011B\u0159it \u00FAhel n\u00E1b\u011Bhu (angle-of-attack, AOA), \u00FAhel vybo\u010Den\u00ED (angle-of-sideslip, AOS) a rychlost letu (air-speed). P\u0159\u00EDpadn\u011B je mo\u017En\u00E9 zkombinovat m\u011B\u0159en\u00ED AOA a AOS na jednu veli\u010Dinu, kter\u00E1 je pot\u00E9 m\u011B\u0159ena s v\u011Bt\u0161\u00ED p\u0159esnost\u00ED - dvojn\u00E1sobn\u00E1 citlivost. Modul tak umo\u017E\u0148uje porovnat digit\u00E1ln\u00ED v\u00FDpo\u010Det s analogov\u00FDm v\u00FDpo\u010Dtem, kter\u00FD je realizovan\u00FD pomoc\u00ED diferenci\u00E1ln\u00EDho opera\u010Dn\u00EDho zesilova\u010De. V\u0161echny uveden\u00E9 veli\u010Diny jsou na digit\u00E1ln\u00ED \u00FAdaj p\u0159ev\u00E1d\u011Bny na z\u00E1klad\u011B m\u011B\u0159en\u00ED tlakov\u00E9 diference p\u0159iv\u00E1d\u011Bn\u00E9 k modulu z Pitot-statick\u00E9 sondy. Za\u0159\u00EDzen\u00ED poskytuje na v\u00FDstupu parametr koeficient deltaP/Pc bu\u010F pro jeden \u00FAhel m\u011B\u0159en\u00FD p\u0159esn\u011Bj\u0161\u00ED metodou, nebo pro dva \u00FAhly m\u011B\u0159en\u00E9 klasickou metodou. P\u0159epo\u010Det na stupn\u011B je realizov\u00E1n na z\u00E1klad\u011B parametr\u016F sn\u00EDmac\u00ED sondy, kde se dosahuje p\u0159ednost 0.5\u00B0 pro prvn\u00ED p\u0159\u00EDpad a 1\u00B0 pro druh\u00E9 zapojen\u00ED. M\u011B\u0159en\u00E1 data jsou v n\u011Bkolika m\u00F3dech odes\u00EDl\u00E1na na sb\u011Brnici CAN."@cs . "AOAaAOSaSPEED is a functional prototype that with help of MEMS pressure sensors allows measurement of angle-of-attack, angle-of-sideslip and air-speed. The device allows combination of AOA and AOS measurement to sample just one quantity but with doubled precision. The module allows comparison of the digital calculation with its analogue alternative that is performed by a differential amplifier. All the measured quantities are converted to the digital values based on pressure difference measurement fed from a Pitot-static Probe. The device provides deltaP/Pc coefficient even for one angle measured by more precise method or two angles measured in a classic way. Related angles are calculated with respect to a used probe parameters where 0.5\u00B0 precision is reached in the first case and 1\u00B0 in the second one. Data re transmitted over a CAN bus."@en . . . . . . . "Modul m\u011B\u0159en\u00ED rychlosti letu, \u00FAhlu n\u00E1b\u011Bhu a \u00FAhlu vybo\u010Den\u00ED" . . . . "An Air-speed, Angle-of-attack and Angle-of-sideslip Measurement Module"@en . . "5"^^ . . "AOAaAOSaSPEED je funk\u010Dn\u00ED vzorek, kter\u00FD umo\u017E\u0148uje za pou\u017Eit\u00ED MEMS senzor\u016F tlaku m\u011B\u0159it \u00FAhel n\u00E1b\u011Bhu (angle-of-attack, AOA), \u00FAhel vybo\u010Den\u00ED (angle-of-sideslip, AOS) a rychlost letu (air-speed). P\u0159\u00EDpadn\u011B je mo\u017En\u00E9 zkombinovat m\u011B\u0159en\u00ED AOA a AOS na jednu veli\u010Dinu, kter\u00E1 je pot\u00E9 m\u011B\u0159ena s v\u011Bt\u0161\u00ED p\u0159esnost\u00ED - dvojn\u00E1sobn\u00E1 citlivost. Modul tak umo\u017E\u0148uje porovnat digit\u00E1ln\u00ED v\u00FDpo\u010Det s analogov\u00FDm v\u00FDpo\u010Dtem, kter\u00FD je realizovan\u00FD pomoc\u00ED diferenci\u00E1ln\u00EDho opera\u010Dn\u00EDho zesilova\u010De. V\u0161echny uveden\u00E9 veli\u010Diny jsou na digit\u00E1ln\u00ED \u00FAdaj p\u0159ev\u00E1d\u011Bny na z\u00E1klad\u011B m\u011B\u0159en\u00ED tlakov\u00E9 diference p\u0159iv\u00E1d\u011Bn\u00E9 k modulu z Pitot-statick\u00E9 sondy. Za\u0159\u00EDzen\u00ED poskytuje na v\u00FDstupu parametr koeficient deltaP/Pc bu\u010F pro jeden \u00FAhel m\u011B\u0159en\u00FD p\u0159esn\u011Bj\u0161\u00ED metodou, nebo pro dva \u00FAhly m\u011B\u0159en\u00E9 klasickou metodou. P\u0159epo\u010Det na stupn\u011B je realizov\u00E1n na z\u00E1klad\u011B parametr\u016F sn\u00EDmac\u00ED sondy, kde se dosahuje p\u0159ednost 0.5\u00B0 pro prvn\u00ED p\u0159\u00EDpad a 1\u00B0 pro druh\u00E9 zapojen\u00ED. M\u011B\u0159en\u00E1 data jsou v n\u011Bkolika m\u00F3dech odes\u00EDl\u00E1na na sb\u011Brnici CAN." . "[2889E48F3633]" . . "Low-cost" . "5"^^ .