Development of MEMS sensors for aircraft control systems

Pleiades Publishing Ltd - Tập 2 - Trang 59-62 - 2011
A. G. Kuznetsov1, Z. S. Abutidze2, B. I. Portnov1, V. I. Galkin1, A. A. Kalik1
1Moscow Institute of Electromechanics and Automatics, Moscow, Russia
2Aviapribor Holding, ZAO Aviapribor, Moscow, Russia

Tóm tắt

Results of development of MEMS sensors for control systems of Tu-204, Il-96, Tu-334, Yak-130 aircraft performed at the Moscow Institute of Electromechanics and Automatics are presented. Design features and obtained technical parameters of the developed devices are considered. Prospects for their application in a wide range of aircraft are shown.

Tài liệu tham khảo

Peshekhonov, V.G., et al., Test Results of an RR-Type Micromechanical Gyroscope, Proc. 17th St. Petersburg Conf. on Integrated Navigation Systems, St. Petersburg, 2010, pp. 9–17. Suminov, V.M. and Galkin, V.I., State and Prospects of MEMS Gyro Development, in Nauchn. trudy MATI (Proc. MATI), Tsiolkovskii Russian State Technological University, no. 10(82), Moscow, MATI, 2006, pp. 154–160. iVRU-SBA1-C167 Vertical Reference Unit with High Rate MEMS Gyros, MEMS Accelerometers and Integrated Strapdown Processor, iMAR GmbH, http://www.imar-navigation.de. GPS Integrated Inertial Navigation Unit, ATAIR Aerospace Inc. Collins AHS-3000, Attitude Heading Reference System, www.rockwellcollins.com. Micromachined Vibrating Beam Multisensor (MVBM), Kearfott Guidance & Navigation Corporation, www.kearfott.com. On Track with MEMS, Avionics Magazine, January, 2006, pp. 42–45, www.avionicsmagazine.com. Inertial MEMS System Application, RTO-LS-232 (2004) Preprints. MEMS Gyros, Silicon Sensing Systems, [email protected]. Abutidze, Z.S., Kuznetsov, A.G., Galkin, V.I., and Kalik, A.A.., Patent no. 80230, Single-Axis MEMS Gyro, Byulleten, 2009, no. 3. Abutidze, Z.S., Kuznetsov, A.G., Galkin, V.I., and Kalik, A.A.., Patent no. 80157, Three-Axis MEMS Motion Parameter Meter, Byulleten, 2009, no. 3.