Analysis on the Errors Caused by the Axial Acceleration of a Single Mass Capacitive Vibratory Micro-machined Gyro and Design of High-order Low-pass Filtering Module
In order to estimate and get the flight attitude, trajectory, launching speed, ejection altitude, landing point, landing speed and displacement, etc. of aircraft, parameters of six degree of freedom inertial measurement unit are usually acquired to establish the settlement data base in the design an...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
IFSA Publishing, S.L.
2014-02-01
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| Series: | Sensors & Transducers |
| Subjects: | |
| Online Access: | http://www.sensorsportal.com/HTML/DIGEST/february_2014/Vol_165/P_RP_0079.pdf |