Flight testing of control allocation for elevator actuator fault in small UAV
Actuators; Control surfaces; Elevators; Fault detection; Fighter aircraft; Flight control systems; Unmanned aerial vehicles (UAV); Actuator fault; Control allocation; Control techniques; Fault accommodation; Flight endurance; Simulation Design; Single components; Unmanned aircrafts; Aircraft control
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Institute of Electrical and Electronics Engineers Inc.
2023
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my.uniten.dspace-233172023-05-29T14:39:26Z Flight testing of control allocation for elevator actuator fault in small UAV Sahwee Z. Mahmood A.S. Rahman N.A. Sahari K.S.M. 55524079500 57193427529 9338388000 57218170038 Actuators; Control surfaces; Elevators; Fault detection; Fighter aircraft; Flight control systems; Unmanned aerial vehicles (UAV); Actuator fault; Control allocation; Control techniques; Fault accommodation; Flight endurance; Simulation Design; Single components; Unmanned aircrafts; Aircraft control Final validation of new control technique for any air vehicle must be conducted through flight testing. It is the most critical phase of the research work where it validates and provides real world feedback on the theoretical and simulation design. On the other hand, an unmanned aircraft as presented in this work is highly complex systems; a single component failure can lead to potentially dangerous consequences. The objective of this paper is to present the flight test result on the investigation on using alternate control surface for a control allocation of pitch control transition from elevator to stabilator of a small UAV. There were fourty flight tests have been performed and from the analysis, the proposed method is feasible to be used without affecting flight endurance and characteristics during flight control transition. The alternate control surface accommodation technique proves to promise higher reliability in case of faulty on-board actuator. � 2016 IEEE. Final 2023-05-29T06:39:26Z 2023-05-29T06:39:26Z 2017 Conference Paper 10.1109/ICCAIS.2016.7822466 2-s2.0-85013790906 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85013790906&doi=10.1109%2fICCAIS.2016.7822466&partnerID=40&md5=b3c683b68c2c882115873536a3dc803d https://irepository.uniten.edu.my/handle/123456789/23317 7822466 232 237 Institute of Electrical and Electronics Engineers Inc. Scopus |
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| description |
Actuators; Control surfaces; Elevators; Fault detection; Fighter aircraft; Flight control systems; Unmanned aerial vehicles (UAV); Actuator fault; Control allocation; Control techniques; Fault accommodation; Flight endurance; Simulation Design; Single components; Unmanned aircrafts; Aircraft control |
| author2 |
55524079500 |
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55524079500 Sahwee Z. Mahmood A.S. Rahman N.A. Sahari K.S.M. |
| format |
Conference Paper |
| author |
Sahwee Z. Mahmood A.S. Rahman N.A. Sahari K.S.M. |
| spellingShingle |
Sahwee Z. Mahmood A.S. Rahman N.A. Sahari K.S.M. Flight testing of control allocation for elevator actuator fault in small UAV |
| author_sort |
Sahwee Z. |
| title |
Flight testing of control allocation for elevator actuator fault in small UAV |
| title_short |
Flight testing of control allocation for elevator actuator fault in small UAV |
| title_full |
Flight testing of control allocation for elevator actuator fault in small UAV |
| title_fullStr |
Flight testing of control allocation for elevator actuator fault in small UAV |
| title_full_unstemmed |
Flight testing of control allocation for elevator actuator fault in small UAV |
| title_sort |
flight testing of control allocation for elevator actuator fault in small uav |
| publisher |
Institute of Electrical and Electronics Engineers Inc. |
| publishDate |
2023 |
| _version_ |
1806428168792309760 |