Design of a MEMS piezoresistive differential pressure sensor with small thermal hysteresis for air data modules

Author:

Song Jin Woo1ORCID,Lee Jang-Sub2,An Jun-Eon3,Park Chan Gook4

Affiliation:

1. BK21Plus Transformative Training Program for Creative Mechanical and Aerospace Engineers, Department of Mechanical and Aerospace Engineering, Seoul National University, 1 Gwanak-ro, Gwanak, Seoul 151-744, South Korea

2. Microinfinity Co., Ltd., 109 Gwanggyo, Suwon, Gyeonggi 443-270, South Korea

3. Agency for Defense Development, Bugyuseong-daero 488 beon-gil, Yuseong, Daejeon 305-152, South Korea

4. Department of Mechanical and Aerospace Engineering, Seoul National University, 1 Gwanak-ro, Gwanak, Seoul 151-744, South Korea

Funder

Agency for Defense Development (ADD)

Publisher

AIP Publishing

Subject

Instrumentation

Reference57 articles.

1. A. Cho, Y.S. Kang, B.J. Park, C.S. Yoo, and S.O. Koo, in 2012 12th International Conference on Control, Automation and Systems (ICCAS), (2012), pp. 433–436.

2. An Improvement to an Algorithm for Computing Aircraft Reference Altitude

3. W. Gracey, “Measurement of aircraft speed and altitude,” Report, DTIC Document, 1980.

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