Integrating Bird Strike Risk Information into the Airport Management System

Isabel Metz, M. Freese, T. Pett, S. Schier

Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

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The calibration of Angular Accelerometers requires a controlled test with a known accel- eration pro_le. However, current turn-tables have been designed primarily for generating a constant rotational velocity. To generate a pro_le with varying angular acceleration we propose using constant rotational velocity on the two axes of a 2-axes motion simulator. The proposed sequence was developed to obtain the required rotational acceleration signal quality using only rotational velocity input. The identi_ed pattern is applied to an enve- lope of test conditions, resulting in test matrix. This method provides an alternative means to generate inputs that can be used to calibrate angular accelerometers using calibration hardware that is not primarily designed to provide accurate acceleration inputs.
Original languageEnglish
Title of host publicationProceedings of the 65th German Aerospace Congress
Subtitle of host publicationBraunschweig, Germany
EditorsMarkus Koller
Number of pages9
Publication statusPublished - 2016
Event65th German Aerospace Congress - Braunschweig, Germany
Duration: 13 Sep 201615 Sep 2016
Conference number: 65


Conference65th German Aerospace Congress
Abbreviated titleDLRK2016
Internet address

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