Vibration detection with 100 Hz GPS PVAT during a dynamic flight

authored by: Christian Bischof, Steffen Schön
Abstract: This investigation gives insights into real 100 Hz GPS velocity and acceleration estimates from a position, velocity, acceleration and time (PVAT) extended Kalman filter (EKF) during a highly dynamic flight trial with a Dornier Do 128-6 aircraft. We investigated the accelerations during take-off, landing and wing shaking manoeuvres in order to compare the vibration behaviour of the given aircraft determined by means of GPS against an onboard IMU. We found that 100 Hz GPS acceleration is useful for characterising vibrations and giving valuable insights during highly dynamic flights. Potential latency of 0.12 s and amplitude misestimation of up to 80% w.r.t. the reference amplitude occur that should be determined beforehand in order to correctly interpret the results.
Organisation(s): Institute of Geodesy
Type: Article
Journal: Advances in space research
Volume: 59
Pages: 2779-2793
No. of pages: 15
ISSN: 0273-1177
Publication date: 18.08.2016
Publication status: Published
Peer reviewed: Yes
ASJC Scopus subject areas: Aerospace Engineering, Astronomy and Astrophysics, Geophysics, Atmospheric Science, Space and Planetary Science, General Earth and Planetary Sciences
Electronic version(s): https://doi.org/10.1016/j.asr.2016.08.008 (Access: Closed)
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