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 inCEAS aeronautical journal Vol. 13; no. 1; pp. 199 - 213
Main Authors Dal Borgo, Mattia, Elliott, Stephen J., Ghandchi Tehrani, Maryam, Stothers, Ian M.
Format Journal Article
LanguageEnglish
Published Vienna Springer Vienna 01.01.2022
Springer Nature B.V
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ISSN1869-5582
1869-5590
DOI10.1007/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.
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 LangleyRBGPS World199910552
Huber, P.J., Ronchetti, E.M.: Robust statistics (John Wiley & Sons, 2009). https://doi.org/10.1002/9780470434697
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
Blewitt, G.: Basics of the GPS technique: observation equations (Swedish Land Survey, 1997), pp. 10–54
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
OosteromMBabuskaRVerbruggenHBIEEE transactions on systems, man, and cyberneticsPart C (Applications and Reviews)200232212510.1109/TSMCC.2002.801357
FrankPMAutomatica199026345910.1016/0005-1098(90)90018-D
HengLGaoGWalterTEngePGPS World2011221144
Federal Aviation AdministrationAviation Maintenance Technician Handbook-Airframe (Chapter 13)2018Oklahoma CityUnited States Department of Transportation
Catapult, H.V.M.: Feasibility of an immersive digital twin (2018). Accessed: 2019-11-29
RutledgeDGPS World201021542
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
Oxley, A.: Uncertainties in GPS Positioning: A mathematical discourse, 1st edn. (Academic Press, 2017)
YoungDWSOhlyBSAE Trans.19859488110.4271/851940
LangleyRBGPS World19912745
ZhangTWangFFuWAppl Sci20188686510.3390/app8060865
Zhang, M., Jiang, R.M., Nie, H.: International Journal of Aerospace Engineering (Article ID 1626015), 14 (2016). https://doi.org/10.1155/2016/1626015
LangleyRBGPS World199910360
MarzatJPiet-LahanierHDamongeotFWalterEProceedings of the institution of mechanical engineersPart G201222610132910.1177/0954410011421717https://hal-supelec.archives-ouvertes.fr/hal-00615617
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
BoYYongyuanQYanCMeasurement Sci Technol2006176152210.1088/0957-0233/17/6/033
557_CR16
D Rutledge (557_CR17) 2010; 21
Federal Aviation Administration (557_CR2) 2018
DWS Young (557_CR3) 1985; 94
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RB Langley (557_CR13) 1999; 10
557_CR11
J Marzat (557_CR9) 2012; 226
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L Heng (557_CR15) 2011; 22
Y Bo (557_CR19) 2006; 17
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RB Langley (557_CR14) 1999; 10
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T Zhang (557_CR18) 2018; 8
M Oosterom (557_CR8) 2002; 32
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
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– volume-title: Aviation Maintenance Technician Handbook-Airframe (Chapter 13)
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  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
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  publication-title: SAE Trans.
  doi: 10.4271/851940
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  publication-title: GPS World
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Snippet Many safety-critical control systems use multiple redundant sensors to estimate the same controlled signal. If the sensors were to operate perfectly, only a...
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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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