Fast Loss of Effectiveness Detection on a Quadrotor Using Onboard Sensors and a Kalman Estimation Approach

B.A. Strack Van Schijndel*, S. Sun, C.C. de Visser

*Corresponding author for this work

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

6 Citations (SciVal)
89 Downloads (Pure)

Abstract

This paper presents a novel method for fast and robust detection of actuator failures on quadrotors. The proposed algorithm has very little model dependency. A Kalman estimator estimates a stochastic effectiveness factor for every actuator, using only onboard RPM, gyro and accelerometer measurements. Then, a hypothesis test identifies the failed actuator. This algorithm is validated online in real-time, also as part of an active fault tolerant control system. Loss of actuator effectiveness is induced by ejecting the propellers from the motors. The robustness of this algorithm is further investigated offline over a range of parameter settings by replaying real flight data containing 26 propeller ejections. The detection delays are found to be in the 30∼130 ms range, without missed detections or false alarms occurring.
Original languageEnglish
Title of host publication2023 International Conference on Unmanned Aircraft Systems, ICUAS 2023
PublisherIEEE
Number of pages8
ISBN (Electronic)9798350310375
DOIs
Publication statusPublished - 2023
Event2023 International Conference on Unmanned Aircraft Systems, ICUAS 2023 - Warsaw, Poland
Duration: 6 Jun 20239 Jun 2023

Conference

Conference2023 International Conference on Unmanned Aircraft Systems, ICUAS 2023
Country/TerritoryPoland
CityWarsaw
Period6/06/239/06/23

Bibliographical note

Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care
Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.

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