Abstract
Being motivated by ceiling inspection applications via unmanned aerial vehicles (UAVs) which require close proximity flight to surfaces, a systematic control approach enabling safe and accurate close proximity flight is proposed in this work. There are two main challenges for close proximity flights: (i) the trust characteristics varies drastically for the different distance from the ceiling which results in a complex nonlinear dynamics; (ii) the system needs to consider physical and environmental constraints to safely fly in close proximity. To address these challenges, a novel framework consisting of a constrained optimization-based force estimation and an optimization-based nonlinear controller is proposed. Experimental results illustrate that the performance of the proposed control approach can stabilize UAV down to 1 cm distance to the ceiling. Furthermore, we report that the UAV consumes up to 12.5% less power when it is operated 1 cm distance to ceiling, which is promising potential for more battery-efficient inspection flights.
Original language | English |
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Title of host publication | 2019 IEEE/RSJ International Conference on Intelligent Robots and Systems, IROS 2019 |
Publisher | Institute of Electrical and Electronics Engineers (IEEE) |
Pages | 2813-2819 |
Number of pages | 7 |
ISBN (Electronic) | 9781728140049 |
DOIs | |
Publication status | Published - Nov 2019 |
Event | 2019 IEEE/RSJ International Conference on Intelligent Robots and Systems, IROS 2019 - Macau, China Duration: 3 Nov 2019 → 8 Nov 2019 |
Publication series
Name | IEEE International Conference on Intelligent Robots and Systems |
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ISSN (Print) | 2153-0858 |
ISSN (Electronic) | 2153-0866 |
Conference
Conference | 2019 IEEE/RSJ International Conference on Intelligent Robots and Systems, IROS 2019 |
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Country/Territory | China |
City | Macau |
Period | 3/11/19 → 8/11/19 |
Bibliographical note
Funding Information:ACKNOWLEDGMENT The authors wish to thank for conducting the research work with support from the Energy Research Institute @ NTU (ERI@N) and NTU internal grant for the project on Large Vertical Take-Off and Landing (VTOL) Research Platform: Prototype development and demonstration (NTU internal funding).
Publisher Copyright:
© 2019 IEEE.