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Author Adiprawita, Widyawardana ♦ Ahmad, Adang Suwandi ♦ Semibiring, Jaka
Source arXiv.org
Content type Text
File Format PDF
Date of Submission 2008-04-24
Language English
Subject Domain (in DDC) Computer science, information & general works
Subject Keyword Computer Science - Robotics ♦ B.4.4 ♦ cs
Abstract This 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.
Description Reference: Proceedings of the International Conference on Intelligent Unmanned System (ICIUS 2007), Bali, Indonesia, October 24-25, 2007, Paper No. ICIUS2007-A009
Educational Use Research
Learning Resource Type Article
Page Count 7


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