"A combined system for angle of attack and angle of sideslip measurement"@en . "A combined system for angle of attack and angle of sideslip measurement"@en . "21230" . "Pa\u010Des, Pavel" . "RIV/68407700:21230/10:00167993" . . "M\u011B\u0159en\u00ED \u00FAhelu n\u00E1b\u011Bhu a vybo\u010Den\u00ED v rozsahu -20 - 20\u00B0, s p\u0159esnost\u00ED +/- 1\u00B0. Vlastn\u00EDkem v\u00FDsledku je \u010CVUT v Praze, I\u010C 68407700." . . "smart probe; angle of attack; angle of sideslip; double amplitude measurement method"@en . "\u00DAspora v\u00E1hy a ceny a zv\u00FD\u0161en\u00ED spolehlivosti oproti k\u0159id\u00E9lkov\u00FDm \u0159e\u0161en\u00EDm" . "RIV/68407700:21230/10:00167993!RIV11-MSM-21230___" . "AOAaAOS01" . "Lab. 051" . . "[EBED82A1F6AB]" . "266660" . . "Za\u0159\u00EDzen\u00ED slou\u017E\u00ED pro m\u011B\u0159en\u00ED orientace proudu vzduchu nab\u00EDhaj\u00EDc\u00EDho na m\u011B\u0159en\u00FD objekt. P\u0159evod vektoru nab\u00EDhaj\u00EDc\u00EDho proudu vzduchu pracuje na principu m\u011B\u0159en\u00ED tlakov\u00E9 diference, kter\u00E1 je m\u011B\u0159ena pomoc\u00ED MEMS senzor\u016F tlaku. V\u00FDstupn\u00ED elektrick\u00FD sign\u00E1l, je d\u00E1le zpracov\u00E1n a vyhodnocen pomoc\u00ED elektroniky %22smart%22 senzoru. Za\u0159\u00EDzen\u00ED obsahuje unik\u00E1tn\u00ED propojen\u00ED senzorov\u00FDch vstup\u016F, kter\u00E9 umo\u017E\u0148uje dos\u00E1hnout dvojn\u00E1sobn\u00E9 velikosti v\u00FDstupn\u00ED hodnoty pomoc\u00ED dvou asymetricky zapojen\u00FDch senzor\u016F. FVZ m\u011B\u0159\u00ED n\u00E1sleduj\u00EDc\u00ED parametry: \u00DAhel n\u00E1b\u011Bhu v rozsahu -20 - 20\u00B0. \u00DAhel vybo\u010Den\u00ED v rozsahu -20 - 20\u00B0. Navr\u017Een\u00E9 \u0159e\u0161en\u00ED dopl\u0148uje syst\u00E9m aerometrick\u00E9ho po\u010D\u00EDta\u010De o detekci a indikaci mo\u017Enosti ztr\u00E1ty vztlaku p\u0159i nestandardn\u00EDch letov\u00FDch re\u017Eimech na letadle. Za\u0159\u00EDzen\u00ED disponuje v\u00FDstupem ve form\u00E1tu CAN a p\u0159esnost\u00ED 1\u00B0. FVZ je um\u00EDst\u011Bn v LAB051, a vznikl na z\u00E1klad\u011B d\u00EDl\u010D\u00EDho \u00FAkolu 2 %22Mikrominiaturizace senzor\u016F a syst\u00E9m\u016F%22 VZ MSM6840770015. C\u00EDlem je ov\u011B\u0159ov\u00E1n\u00ED technologie MEMS senzor\u016F extr\u00E9mn\u011B tvrd\u00FDch" . . . "Kombinovan\u00FD syst\u00E9m m\u011B\u0159en\u00ED \u00FAhlu n\u00E1b\u011Bhu a \u00FAhlu vybo\u010Den\u00ED"@cs . . "Kombinovan\u00FD syst\u00E9m m\u011B\u0159en\u00ED \u00FAhlu n\u00E1b\u011Bhu a \u00FAhlu vybo\u010Den\u00ED" . . . "Z(MSM6840770015)" . . . . "3"^^ . . "Kombinovan\u00FD syst\u00E9m m\u011B\u0159en\u00ED \u00FAhlu n\u00E1b\u011Bhu a \u00FAhlu vybo\u010Den\u00ED"@cs . "Kombinovan\u00FD syst\u00E9m m\u011B\u0159en\u00ED \u00FAhlu n\u00E1b\u011Bhu a \u00FAhlu vybo\u010Den\u00ED" . . . . . . . "Draxler, Karel" . "Za\u0159\u00EDzen\u00ED slou\u017E\u00ED pro m\u011B\u0159en\u00ED orientace proudu vzduchu nab\u00EDhaj\u00EDc\u00EDho na m\u011B\u0159en\u00FD objekt. P\u0159evod vektoru nab\u00EDhaj\u00EDc\u00EDho proudu vzduchu pracuje na principu m\u011B\u0159en\u00ED tlakov\u00E9 diference, kter\u00E1 je m\u011B\u0159ena pomoc\u00ED MEMS senzor\u016F tlaku. V\u00FDstupn\u00ED elektrick\u00FD sign\u00E1l, je d\u00E1le zpracov\u00E1n a vyhodnocen pomoc\u00ED elektroniky %22smart%22 senzoru. Za\u0159\u00EDzen\u00ED obsahuje unik\u00E1tn\u00ED propojen\u00ED senzorov\u00FDch vstup\u016F, kter\u00E9 umo\u017E\u0148uje dos\u00E1hnout dvojn\u00E1sobn\u00E9 velikosti v\u00FDstupn\u00ED hodnoty pomoc\u00ED dvou asymetricky zapojen\u00FDch senzor\u016F. FVZ m\u011B\u0159\u00ED n\u00E1sleduj\u00EDc\u00ED parametry: \u00DAhel n\u00E1b\u011Bhu v rozsahu -20 - 20\u00B0. \u00DAhel vybo\u010Den\u00ED v rozsahu -20 - 20\u00B0. Navr\u017Een\u00E9 \u0159e\u0161en\u00ED dopl\u0148uje syst\u00E9m aerometrick\u00E9ho po\u010D\u00EDta\u010De o detekci a indikaci mo\u017Enosti ztr\u00E1ty vztlaku p\u0159i nestandardn\u00EDch letov\u00FDch re\u017Eimech na letadle. Za\u0159\u00EDzen\u00ED disponuje v\u00FDstupem ve form\u00E1tu CAN a p\u0159esnost\u00ED 1\u00B0. FVZ je um\u00EDst\u011Bn v LAB051, a vznikl na z\u00E1klad\u011B d\u00EDl\u010D\u00EDho \u00FAkolu 2 %22Mikrominiaturizace senzor\u016F a syst\u00E9m\u016F%22 VZ MSM6840770015. C\u00EDlem je ov\u011B\u0159ov\u00E1n\u00ED technologie MEMS senzor\u016F extr\u00E9mn\u011B tvrd\u00FDch"@cs . "2"^^ . . "The device measures its orientation with regards to the ambient airstream. The vector of the ambient airstream is transformed to pressure differences that are converted into electric signals by MEMS pressure sensors whose outputs are converted and evaluated by a smart sensor. The system uses a unique sensor interconnection that allows two times higher output signal, in comparison with a single sensor, by an asymmetric interconnection of sensors. The functional prototype allows measurement of these parameters: Angle of Attack -20 - 20\u00B0 ( 1\u00B0). Angle of Sideslip -20 - 20\u00B0 ( 1\u00B0). This device can complement an air data computer by a set of quantities used for stall warning detection and signalization of non standard regimes of small airplanes. Functional prototype is result of MSM6840770015, partial task #2 %22Microminiaturization of sensors and systems %22"@en . "Va\u0161ko, O." . .