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M. Napolitano (2005)
Development of Formation Flight Control Algorithms Using 3 YF-22 Flying Models
K. Valavanis, G. Vachtsevanos (2015)
UAV Health Management Issues: Introduction
C. Belcastro, Steven Jacobson (2010)
Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control Accidents
M. Perhinschi, H. Moncayo (2018)
Artificial Immune System for Comprehensive and Integrated Aircraft Abnormal Conditions Management
Ghassan Al-Sinbol, M. Perhinschi (2016)
Generation of Power Plant Artificial Immune System Using the Partition of the Universe ApproachInternational review of automatic control, 9
M. Perhinschi, H. Moncayo, D. Azzawi (2014)
Integrated Immunity-Based Framework for Aircraft Abnormal Conditions ManagementJournal of Aircraft, 51
S. Sanchez, M. Perhinschi, H. Moncayo, M. Napolitano, Jennifer Davis, M. Fravolini (2009)
In-Flight Actuator Failure Detection and Identification for a Reduced Size UAV Using the Artificial Immune System Approach
M. Perhinschi, M. Napolitano, G. Campa, B. Seanor, S. Gururajan, Yu Gu (2007)
Development of Fault-Tolerant Flight Control Laws for the WVU YF-22 Model Aircraft
Aline Kraemer, E. Villani (2019)
On the gap between aircraft FDI methods in industry and academy: challenges and directionsAIAA Scitech 2019 Forum
S. Hansen, M. Blanke, Jens Adrian (2012)
Fault Diagnosis and Fault Handling for Autonomous Aircraft
Ghassan Al-Sinbol, M. Perhinschi (2017)
Development of an Artificial Immune System for Power Plant Abnormal Condition Detection, Identification, and EvaluationInternational review of automatic control, 10
B. Wilburn, M. Perhinschi, H. Moncayo, O. Karas, J. Wilburn (2013)
Unmanned aerial vehicle trajectory tracking algorithm comparison, 1
S. Fekri, D. Gu, I. Postlethwaite (2009)
Lateral imbalance detection on a UAV based on multiple modelsProceedings of the 48h IEEE Conference on Decision and Control (CDC) held jointly with 2009 28th Chinese Control Conference
H. Moncayo, M. Perhinschi, Jennifer Davis (2010)
Aircraft Failure Detection and Identification Using an Immunological Hierarchical Multiself StrategyJournal of Guidance Control and Dynamics, 33
H. Moncayo, M. Perhinschi, Jennifer Davis (2010)
Artificial Immune System – Based Aircraft Failure Evaluation over Extended Flight EnvelopeJournal of Guidance Control and Dynamics, 34
R. Khan, R. Hill, C. Bil (2011)
Fault tolerant flight control system design for unmanned air vehicles
Mohanad Alnuaimi, M. Perhinschi, Ghassan Al-Sinbol (2019)
Immunity-Based Framework for Autonomous Flight in GNSS-Denied EnvironmentInternational Review of Aerospace Engineering, 12
M. Perhinschi, M. Napolitano, G. Campa, B. Seanor, J. Burken, R. Larson (2006)
An adaptive threshold approach for the design of an actuator failure detection and identification schemeIEEE Transactions on Control Systems Technology, 14
F. González, D. Dasgupta (2003)
A study of artificial immune systems applied to anomaly detection
M. Perhinschi, B. Wilburn, J. Wilburn, H. Moncayo, O. Karas (2013)
Simulation Environment for UAV Fault Tolerant Autonomous Control Laws Development, 1
M. Perhinschi, H. Moncayo, B. Wilburn, J. Wilburn, O. Karas, A. Bartlett (2014)
Neurally-augmented immunity-based detection and identification of aircraft sub-system failuresThe Aeronautical Journal (1968), 118
(2018)
FAA aerospace forecast, fiscal years 2019-2039
F. Bateman, H. Noura, M. Ouladsine (2011)
Active Fault Diagnosis and Major Actuator Failure Accommodation: Application to a UAV
A. Ortiz, N. Neogi (2008)
A Dynamic Threshold Approach to Fault Detection in Uninhabited Aerial Vehicles
A. Togayev, M. Perhinschi, H. Moncayo, D. Azzawi, Andres Perez (2017)
Immunity-based accommodation of aircraft subsystem failuresAircraft Engineering and Aerospace Technology, 89
H. Moncayo, M. Perhinschi, J. Davis (2011)
Aircraft failure detection and identification over an extended flight envelope using an artificial immune systemThe Aeronautical Journal (1968), 115
An artificial immune system (AIS) for the detection and identification of abnormal operational conditions affecting an unmanned air vehicle (UAV) is developed using the partition of the universe approach. The performance of the proposed methodology is assessed through simulation within the West Virginia University (WVU) unmanned aerial system (UAS) simulation environment.Design/methodology/approachAn AIS is designed and generated for a fixed wing UAV using data from the WVU UAS simulator. A novel partition of the universe approach augmented with the hierarchical multiself strategy is used to define the self, within the AIS paradigm. Several 2-dimensional and 3-dimensional commanded trajectories are simulated under normal and abnormal conditions affecting actuators and sensors. Data recorded are used to build the AIS and develop an abnormal condition detection and identification scheme for the two categories of subsystems. The performance of the methodology is evaluated in terms of detection and identification rates, false alarms and decision times.FindingsThe proposed methodology for UAV abnormal condition detection and identification has the potential to support a comprehensive and integrated solution to the problem of aircraft subsystem health management. The novel partition of the universe approach has been proven to be a promising alternative to the previously investigated clustering methods by providing similar or better performance for the cases investigated.Research limitations/implicationsThe promising results obtained within this research effort motivate further investigation and extension of the proposed methodology toward a complete system health management process, including abnormal condition evaluation and accommodation.Practical implicationsThe use of the partition of the universe approach for AIS generation may potentially represent a valuable alternative to current clustering methods within the AIS paradigm. It can facilitate a simpler and faster implementation of abnormal condition detection and identification schemes.Originality/valueIn this paper, a novel method for AIS generation, the partition of the universe approach, is formulated and applied for the first time for the development of abnormal condition detection and identification schemes for UAVs. This approach is computationally less expensive and mitigates some of the issues related to the typical clustering approaches. The implementation of the proposed approach can potentially enhance the robustness of UAS for safety purposes.
International Journal of Intelligent Unmanned Systems – Emerald Publishing
Published: Oct 12, 2021
Keywords: UAS; Abnormal conditions detection and identification; Artificial immune system; System health management
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