Automated Flight Test and System Identification for Rotary Wing Small Aerial Platform using Frequency Responses Analysis

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dc.creatorAdiprawita, Widyawardana
dc.creatorAhmad, Adang Suwandi
dc.creatorSemibiring, Jaka
dc.date2008-04-24
dc.date.accessioned2026-07-07T09:34:57Z
dc.date.available2026-07-07T09:34:57Z
dc.descriptionThis paper proposes an autopilot system that can be used to control the small scale rotorcraft during the flight test for linear-frequency-domain system identification. The input frequency swept is generated automatically as part of the autopilot control command. Therefore the bandwidth coverage and consistency of the frequency swept is guaranteed to produce high quality data for system identification. Beside that we can set the safety parameter during the flight test (maximum roll or pitch value, minimum altitude, etc) so the safety of the whole flight test is guaranteed. This autopilot for automated flight test will be tested using hardware in the loop simulator for hover flight condition.
dc.descriptionUploaded by ICIUS2007 Conference Organizer on behalf of the author(s). 7 pages, 15 figures
dc.identifierhttps://arxiv.org/abs/0804.3881
dc.identifierhttp://arxiv.org/abs/0804.3881
dc.identifierProceedings of the International Conference on Intelligent Unmanned System (ICIUS 2007), Bali, Indonesia, October 24-25, 2007, Paper No. ICIUS2007-A009
dc.identifier.urihttp://salesiana.dossiersoluciones.com/handle/123456789/159678
dc.subjectRobotics
dc.subjectB.4.4
dc.titleAutomated Flight Test and System Identification for Rotary Wing Small Aerial Platform using Frequency Responses Analysis
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