Virtual sensing of wheel direction from redundant sensors in aircraft ground-steering systems
Many safety-critical control systems use multiple redundant sensors to estimate the same controlled signal. If the sensors were to operate perfectly, only a subset of them would need to be used for the estimation. In practice, however, the sensors are subject to uncertainty, minor or major faults an...
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Published in | CEAS aeronautical journal Vol. 13; no. 1; pp. 199 - 213 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Vienna
Springer Vienna
01.01.2022
Springer Nature B.V |
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ISSN | 1869-5582 1869-5590 |
DOI | 10.1007/s13272-021-00557-z |
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Abstract | Many safety-critical control systems use multiple redundant sensors to estimate the same controlled signal. If the sensors were to operate perfectly, only a subset of them would need to be used for the estimation. In practice, however, the sensors are subject to uncertainty, minor or major faults and their operation may be nonlinear. It is thus important to reliably estimate the controlled signal under these conditions, and also to assess the degree of confidence with which each sensor should be treated. An example of such a control system is the ground-steering control system of an aircraft nose landing gear. A virtual sensing technique is commonly employed, which estimates the steering angle using the measurements of multiple remote displacement sensors. The wheel position is then calculated as a nonlinear function of these sensor outputs. This paper describes how a digital twin of the ground-steering system, in which the effects of uncertainties and faults can be systematically analysed and studied, is used to assess the accuracy and integrity of the steering angle estimation for a number of different estimation algorithms. Two of these algorithms are based on a least-squares approach, while another is a soft-computing technique based on fuzzy logic. These methods are investigated for several scenarios where model uncertainty, measurement noise and sensor faults are included. It is shown that the soft-computing approach is more robust than the least squares based methods under these conditions. |
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AbstractList | Many safety-critical control systems use multiple redundant sensors to estimate the same controlled signal. If the sensors were to operate perfectly, only a subset of them would need to be used for the estimation. In practice, however, the sensors are subject to uncertainty, minor or major faults and their operation may be nonlinear. It is thus important to reliably estimate the controlled signal under these conditions, and also to assess the degree of confidence with which each sensor should be treated. An example of such a control system is the ground-steering control system of an aircraft nose landing gear. A virtual sensing technique is commonly employed, which estimates the steering angle using the measurements of multiple remote displacement sensors. The wheel position is then calculated as a nonlinear function of these sensor outputs. This paper describes how a digital twin of the ground-steering system, in which the effects of uncertainties and faults can be systematically analysed and studied, is used to assess the accuracy and integrity of the steering angle estimation for a number of different estimation algorithms. Two of these algorithms are based on a least-squares approach, while another is a soft-computing technique based on fuzzy logic. These methods are investigated for several scenarios where model uncertainty, measurement noise and sensor faults are included. It is shown that the soft-computing approach is more robust than the least squares based methods under these conditions. |
Author | Ghandchi Tehrani, Maryam Stothers, Ian M. Dal Borgo, Mattia Elliott, Stephen J. |
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References_xml | – reference: YoungDWSOhlyBSAE Trans.19859488110.4271/851940 – reference: Dal Borgo, M., Elliott, S.J., Ghandchi Tehrani, M., Stothers, I.M.: in Proceedings of the 38th IMAC, A Conference and Exposition on Structural Dynamics 2020, vol. 3, ed. by Z. Mao (Springer, Cham, Houston, TX, USA, 2020), vol. 3, pp. 107–118. https://doi.org/10.1007/978-3-030-47638-0_12 – reference: LangleyRBGPS World19912745 – reference: Blewitt, G.: Basics of the GPS technique: observation equations (Swedish Land Survey, 1997), pp. 10–54 – reference: OosteromMBabuskaRVerbruggenHBIEEE transactions on systems, man, and cyberneticsPart C (Applications and Reviews)200232212510.1109/TSMCC.2002.801357 – reference: LangleyRBGPS World199910552 – reference: ZhangTWangFFuWAppl Sci20188686510.3390/app8060865 – reference: FrankPMAutomatica199026345910.1016/0005-1098(90)90018-D – reference: Zhang, M., Jiang, R.M., Nie, H.: International Journal of Aerospace Engineering (Article ID 1626015), 14 (2016). https://doi.org/10.1155/2016/1626015 – reference: Berdjag, D., Zolghadri, A., Cieslak, J., Goupil, P.: in Conference on Control and Fault-Tolerant Systems (SysTol) (Nice, France, 2010), pp. 137–142. https://doi.org/10.1109/SYSTOL.2010.5675993 – reference: MarzatJPiet-LahanierHDamongeotFWalterEProceedings of the institution of mechanical engineersPart G201222610132910.1177/0954410011421717https://hal-supelec.archives-ouvertes.fr/hal-00615617 – reference: Dal Borgo, M., Elliott, S.J., Ghandchi Tehrani, M., Stothers, I.M.: in Proceedings of the 26th International Congress on Sound and Vibration (ICSV26) (Canadian Acoustical Association, Montreal, Canada, 2019), pp. 1–8 – reference: Currey, N.S.: Aircraft Landing Gear Design: Principles and Practices. AIAA Education Series (American Institute of Aeronautics and Astronautics, Washington, DC, USA, 1988). https://doi.org/10.2514/4.861468 – reference: Federal Aviation AdministrationAviation Maintenance Technician Handbook-Airframe (Chapter 13)2018Oklahoma CityUnited States Department of Transportation – reference: HengLGaoGWalterTEngePGPS World2011221144 – reference: Catapult, H.V.M.: Feasibility of an immersive digital twin (2018). Accessed: 2019-11-29 – reference: Oxley, A.: Uncertainties in GPS Positioning: A mathematical discourse, 1st edn. (Academic Press, 2017) – reference: BoYYongyuanQYanCMeasurement Sci Technol2006176152210.1088/0957-0233/17/6/033 – reference: RutledgeDGPS World201021542 – reference: LangleyRBGPS World199910360 – reference: Huber, P.J., Ronchetti, E.M.: Robust statistics (John Wiley & Sons, 2009). https://doi.org/10.1002/9780470434697 – ident: 557_CR10 doi: 10.1155/2016/1626015 – volume: 10 start-page: 52 issue: 5 year: 1999 ident: 557_CR13 publication-title: GPS World – volume: 32 start-page: 125 issue: 2 year: 2002 ident: 557_CR8 publication-title: Part C (Applications and Reviews) doi: 10.1109/TSMCC.2002.801357 – ident: 557_CR11 – ident: 557_CR21 doi: 10.1002/9780470434697 – ident: 557_CR1 doi: 10.2514/4.861468 – ident: 557_CR16 doi: 10.1016/B978-0-12-809594-2.00001-0 – volume: 22 start-page: 44 issue: 11 year: 2011 ident: 557_CR15 publication-title: GPS World – ident: 557_CR7 doi: 10.1109/SYSTOL.2010.5675993 – volume: 21 start-page: 42 issue: 5 year: 2010 ident: 557_CR17 publication-title: GPS World – ident: 557_CR6 – volume: 17 start-page: 1522 issue: 6 year: 2006 ident: 557_CR19 publication-title: Measurement Sci Technol doi: 10.1088/0957-0233/17/6/033 – volume-title: Aviation Maintenance Technician Handbook-Airframe (Chapter 13) year: 2018 ident: 557_CR2 – volume: 26 start-page: 459 issue: 3 year: 1990 ident: 557_CR20 publication-title: Automatica doi: 10.1016/0005-1098(90)90018-D – volume: 94 start-page: 881 year: 1985 ident: 557_CR3 publication-title: SAE Trans. doi: 10.4271/851940 – volume: 2 start-page: 45 issue: 7 year: 1991 ident: 557_CR12 publication-title: GPS World – volume: 10 start-page: 60 issue: 3 year: 1999 ident: 557_CR14 publication-title: GPS World – ident: 557_CR5 doi: 10.1007/978-3-030-47638-0_12 – volume: 226 start-page: 1329 issue: 10 year: 2012 ident: 557_CR9 publication-title: Part G doi: 10.1177/0954410011421717 – ident: 557_CR4 – volume: 8 start-page: 865 issue: 6 year: 2018 ident: 557_CR18 publication-title: Appl Sci doi: 10.3390/app8060865 |
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SubjectTerms | Aerospace Technology and Astronautics Aircraft Aircraft control Algorithms Computation Control systems Engineering Faults Fuzzy logic Ground based control Landing gear Least squares Noise measurement Original Paper Position measurement Remote sensors Safety critical Sensors Steering Uncertainty |
Title | Virtual sensing of wheel direction from redundant sensors in aircraft ground-steering systems |
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