Browsing Staff publications (SATM) by Author "Ignatyev, Dmitry I."

Browsing Staff publications (SATM) by Author "Ignatyev, Dmitry I."

Sort by: Order: Results:

  • Bayesian calibration for multiple source regression model 
    Ignatyev, Dmitry I.; Shin, Hyo-Sang; Tsourdos, Antonios (Elsevier, 2018-08-20)
    In large variety of practical applications, using information from different sources or different kind of data is a reasonable demand. The problem of studying multiple source data can be represented as a multi-task learning ...
  • Fault detection, isolation and adaptive augmentation for incremental backstepping flight control 
    Ignatyev, Dmitry I.; Shin, Hyo-Sang; Tsourdos, Antonios (Elsevier, 2021-04-14)
    Uncertainties caused by unforeseen malfunctions of the actuator or changes in aircraft behavior could lead to aircraft loss of control during flight. The paper presents a Two-Layer Framework (TLF) augmenting Incremental ...
  • Gaussian process adaptive incremental backstepping flight control 
    Ignatyev, Dmitry I.; Shin, Hyo-Sang; Tsourdos, Antonios (AIAA, 2021-12-29)
    The presence of uncertainties caused by unforeseen malfunctions in the actuation system or changes in aircraft behaviour could lead to aircraft loss of control during flight. The paper proposes almost model-independent ...
  • A global-local meta-modelling technique for model updating 
    Dessena, Gabriele; Ignatyev, Dmitry I.; Whidborne, James F.; Zanotti Fragonara, Luca (Elsevier, 2023-10-09)
    The finite element model updating procedure of large or complex structures is challenging for engineering practitioners and researchers. Iterative methods, such as genetic algorithms and response surface models, have a ...
  • Ground vibration testing of a flexible wing: a benchmark and case study 
    Dessena, Gabriele; Ignatyev, Dmitry I.; Whidborne, James F.; Pontillo, Alessandro; Zanotti Fragonara, Luca (MDPI, 2022-08-10)
    Beam-like flexible structures are of interest in many fields of engineering, particularly aeronautics, where wings are frequently modelled and represented as such. Experimental modal analysis is commonly used to characterise ...
  • Ground vibration testing of a high aspect ratio wing with revolving clamp 
    Dessena, Gabriele; Ignatyev, Dmitry I.; Whidborne, James F.; Pontillo, Alessandro; Zanotti Fragonara, Luca (ICAS, 2022-11-28)
    The advancements in the aeronautical industry and research on materials and manufacturing methods in the last 70 years have been shifting the paradigm of wing design to high aspect ratio flexible wings. These wings can ...
  • Group design project in control engineering: Adapting to COVID-19 pandemic 
    Ignatyev, Dmitry I.; Shin, Hyo-Sang; Zolotas, Argyrios; Tsourdos, Antonios (Elsevier, 2021-11-18)
    Group Design Project (GDP) is a common education strategy in engineering. However, due to the COVID-19 pandemic, GDP cannot be fulfilled in a typical lab condition. The paper describes an example of delivering intensive ...
  • Hybrid terrain traversability analysis in off-road environments 
    Leung, Tiga Ho Yin; Ignatyev, Dmitry I.; Zolotas, Argyrios (IEEE, 2022-03-22)
    There is a significant growth in autonomy level in off-road ground vehicles. However, unknown off-road environments are often challenging due to their unstructured and rough nature. To find a path that the robot can move ...
  • Interplay of unsteady aerodynamics and flight dynamics of transport aircraft in icing conditions 
    Ignatyev, Dmitry I.; Khrabrov, Alexander N.; Kortukova, A. I.; Alieva, D. A.; Sidoryuk, Maria E.; Bazhenov, Sergey G. (Elsevier, 2020-06-11)
    Airframe icing causes significant degradation of aerodynamic characteristics and influences the flight safety. Wind tunnel study of longitudinal steady and unsteady aerodynamic characteristics of a transport aircraft in ...
  • A Kriging approach to model updating for damage detection 
    Dessena, Gabriele; Ignatyev, Dmitry I.; Whidborne, James F.; Zanotti Fragonara, Luca (Springer, 2022-06-16)
    For complex or large structures, the model updating process can be long and tedious and numerical methods can be computationally expensive. Hence, practitioners and researchers often resort to meta-modelling techniques ...
  • Nonlinear analysis for wing rock system with adaptive control 
    Li, Dongyang; Ignatyev, Dmitry I.; Tsourdos, Antonios; Wang, Zhongyuan (AIAA, 2021-12-29)
    Adaptive control has the potential to improve the performance and reliability of aircraft. However, the inherent nonlinearity of adaptive control causes difficulty in stability and robustness verification which is critical ...
  • Nonlinear analysis for wing-rock system with adaptive control 
    Li, Dongyang; Tsourdos, Antonios; Wang, Zhongyuan; Ignatyev, Dmitry I. (AIAA, 2022-07-25)
    Introduction The potential of adaptive control in improving the performance and reliability of control systems attracts researchers and engineers from different disciplines. However, the verification and validation of the ...
  • On-line learning and updating unmanned tracked vehicle dynamics 
    Strawa, Natalia; Ignatyev, Dmitry I.; Zolotas, Argyrios C.; Tsourdos, Antonios (MDPI, 2021-01-15)
    Increasing levels of autonomy impose more pronounced performance requirements for unmanned ground vehicles (UGV). Presence of model uncertainties significantly reduces a ground vehicle performance when the vehicle is ...
  • Region of attraction analysis for adaptive control of wing rock system 
    Li, Dongyang; Ignatyev, Dmitry I.; Tsourdos, Antonios; Wang, Zhongyuan (Elsevier, 2021-11-01)
    This paper introduces a numerical method for region of attraction (ROA) estimation of the adaptive control system in polynomial form. A classical adaptive controller with sigma modification on suppressing the wing rock ...
  • Sparse online Gaussian process adaptation for incremental backstepping flight control 
    Ignatyev, Dmitry I.; Shin, Hyo-Sang; Tsourdos, Antonios (Elsevier, 2023-02-28)
    Presence of uncertainties caused by unforeseen malfunctions in actuation or measurement systems or changes in aircraft behaviour could lead to aircraft loss-of-control during flight. This paper considers sparse online ...
  • Two-layer adaptive augmentation for incremental backstepping flight control of transport aircraft in uncertain conditions 
    Ignatyev, Dmitry I.; Shin, Hyo-Sang; Tsourdos, Antonios (Elsevier, 2020-07-01)
    Presence of uncertainties caused by unforeseen malfunctions in actuation system or changes in aircraft behaviour could lead to aircraft loss-of-control during flight. The paper presents Two-Layer Adaptive augmentation for ...
  • Two-layer on-line parameter estimation for adaptive incremental backstepping flight control for a transport aircraft in uncertain conditions 
    Ignatyev, Dmitry I.; Shin, Hyo-Sang; Tsourdos, Antonios (Elsevier, 2019-11-25)
    Presence of uncertainties caused by unforeseen malfunctions of the actuator or changes in aircraft behavior could lead to aircraft loss of control during flight. The paper presents two-layer parameter estimation procedure ...

Search CERES


Browse

My Account