Searched for: author:"Jatiningrum, D."
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document
Jatiningrum, D. (author)
Fault-Tolerant Flight Control (FTFC) systems reconfigure aircraft flight control laws to help restore a controlled flight and preserve acceptable performance under systemfaults. A typical approach to achieve fault tolerance is using inertial sensor measurementswhich can provide robustness to abrupt changes in the aircraft dynamics. This method...
doctoral thesis 2018
document
Jatiningrum, D. (author), de Visser, C.C. (author), van Paassen, M.M. (author), Mulder, M. (author)
A characterization of an angular accelerometer sensor is performed with a frequency- response experiment. To assess angular accelerometer dynamic properties, a position-based calibration table is utilized to provide the excitation input. The angular accelerometer specifications and calibration table limitations dfine a constrained test envelope...
conference paper 2016
document
Jatiningrum, D. (author), de Visser, C.C. (author), van Paassen, M.M. (author), Mulder, M. (author)
The calibration of Angular Accelerometers requires a controlled test with a known acceleration profile. However, current turn-tables have been designed primarily for generating a constant rotational velocity. To generate a profile with varying angular acceleration we propose using constant rotational velocity on the two axes of a 2-axes motion...
conference paper 2016
document
Jatiningrum, D. (author), De Visser, C.C. (author), Van Paassen, M.M. (author), Mulder, M. (author)
With the role of angular accelerometers in future fault-tolerant flight control systems, an in-depth evaluation of their performance then becomes a critical issue from the perspective of control system design. In this paper, a position-based calibration table is utilized to provide a sufficiently accurate angular acceleration reference in the...
conference paper 2015
Searched for: author:"Jatiningrum, D."
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