Jove
Visualize
Contact Us
JoVE
x logofacebook logolinkedin logoyoutube logo
ABOUT JoVE
OverviewLeadershipBlogJoVE Help Center
AUTHORS
Publishing ProcessEditorial BoardScope & PoliciesPeer ReviewFAQSubmit
LIBRARIANS
TestimonialsSubscriptionsAccessResourcesLibrary Advisory BoardFAQ
RESEARCH
JoVE JournalMethods CollectionsJoVE Encyclopedia of ExperimentsArchive
EDUCATION
JoVE CoreJoVE BusinessJoVE Science EducationJoVE Lab ManualFaculty Resource CenterFaculty Site
Terms & Conditions of Use
Privacy Policy
Policies

Related Concept Videos

Wind Turbine Machine Models01:24

Wind Turbine Machine Models

526
In the growing field of wind energy, incorporating wind turbine models into transient stability analysis is essential. Induction and synchronous machines are the primary models used, with induction machines being prevalent due to their simplicity and reliability.
Induction machines interact through the rotating magnetic field generated by the stator and the rotor. The key parameter is slip, which is the difference between synchronous speed and rotor speed relative to synchronous speed. Slip is...
526
Mechanical Efficiency of Real Machines01:14

Mechanical Efficiency of Real Machines

1.2K
The mechanical efficiency of a machine is a fundamental concept that describes how effectively a machine can convert input work into output work. According to this concept, the efficiency of a machine is equal to the ratio of the output work to the input work. An ideal machine, meaning a machine that has no energy losses, has an efficiency of one. This implies that the input work and the output work are equal.
However, in reality, no machine can be truly ideal, and all of them experience some...
1.2K
Time-Domain Interpretation of PD Control01:07

Time-Domain Interpretation of PD Control

324
Proportional-Derivative (PD) control is a widely used control method in various engineering systems to enhance stability and performance. In a system with only proportional control, common issues include high maximum overshoot and oscillation, observed in both the error signal and its rate of change. This behavior can be divided into three distinct phases: initial overshoot, subsequent undershoot, and gradual stabilization.
Consider the example of control of motor torque. Initially, a positive...
324

You might also read

Related Articles

Articles linked to this work by shared authors, journal, and citation graph.

Sort by
Same author

Simulation and Optimization Design of Inductive Wear Particle Sensor.

Sensors (Basel, Switzerland)·2023
Same author

Segmentation of Online Ferrograph Images with Strong Interference Based on Uniform Discrete Curvelet Transformation.

Sensors (Basel, Switzerland)·2019
Same author

Identification of small-molecule HSF1 amplifiers by high content screening in protection of cells from stress induced injury.

Biochemical and biophysical research communications·2009
Same author

Nanowire transformation by size-dependent cation exchange reactions.

Nano letters·2009
Same author

Effect of haishengsu as an adjunct therapy for patients with advanced renal cell cancer: a randomized and placebo-controlled clinical trial.

Journal of alternative and complementary medicine (New York, N.Y.)·2009
Same author

Identification of inhibitors of HSF1 functional activity by high-content target-based screening.

Journal of biomolecular screening·2009

Related Experiment Video

Updated: Dec 28, 2025

Design and Application of a Fault Detection Method Based on Adaptive Filters and Rotational Speed Estimation for an Electro-Hydrostatic Actuator
06:45

Design and Application of a Fault Detection Method Based on Adaptive Filters and Rotational Speed Estimation for an Electro-Hydrostatic Actuator

Published on: October 28, 2022

2.0K

Aircraft Engine Prognostics Based on Informative Sensor Selection and Adaptive Degradation Modeling with Functional

Bin Zhang1,2, Kai Zheng1, Qingqing Huang3

  • 1School of Advanced Manufacturing Engineering, Chongqing University of Posts and Telecommunications, Chongqing 400065, China.

Sensors (Basel, Switzerland)
|February 14, 2020
PubMed
Summary

This study introduces a new method for aircraft engine prognostics, improving safety and efficiency. It accurately predicts engine degradation by selecting key sensor data and adaptively modeling its health using functional data analysis.

Keywords:
Bayesian inferenceaircraft enginedegradation modelingfunctional principal component analysisprognosticssensor selection

More Related Videos

Data Acquisition Protocol for Determining Embedded Sensitivity Functions
07:46

Data Acquisition Protocol for Determining Embedded Sensitivity Functions

Published on: April 20, 2016

6.4K
A Modeling and Simulation Method for Preliminary Design of an Electro-Variable Displacement Pump
09:04

A Modeling and Simulation Method for Preliminary Design of an Electro-Variable Displacement Pump

Published on: June 1, 2022

3.4K

Related Experiment Videos

Last Updated: Dec 28, 2025

Design and Application of a Fault Detection Method Based on Adaptive Filters and Rotational Speed Estimation for an Electro-Hydrostatic Actuator
06:45

Design and Application of a Fault Detection Method Based on Adaptive Filters and Rotational Speed Estimation for an Electro-Hydrostatic Actuator

Published on: October 28, 2022

2.0K
Data Acquisition Protocol for Determining Embedded Sensitivity Functions
07:46

Data Acquisition Protocol for Determining Embedded Sensitivity Functions

Published on: April 20, 2016

6.4K
A Modeling and Simulation Method for Preliminary Design of an Electro-Variable Displacement Pump
09:04

A Modeling and Simulation Method for Preliminary Design of an Electro-Variable Displacement Pump

Published on: June 1, 2022

3.4K

Area of Science:

  • Aerospace Engineering
  • Mechanical Engineering
  • Data Science

Background:

  • Aircraft engine prognostics are vital for safety, reliability, and operational efficiency.
  • Advancements in sensor technology provide abundant data for engine health monitoring.
  • Effective utilization of multi-sensor data remains a challenge in engine prognostics.

Purpose of the Study:

  • To develop an advanced prognostic approach for aircraft engines.
  • To enhance engine health prediction accuracy by selecting informative sensors and adaptive modeling.
  • To improve aircraft safety and operational efficiency through better prognostics.

Main Methods:

  • Informative sensor selection based on defined metrics.
  • Construction of a health index by fusing selected sensor data.
  • Adaptive degradation modeling using functional principal component analysis (FPCA).
  • Future health prognostication via Bayesian inference.

Main Results:

  • The method effectively identifies and selects the most informative sensors for engine prognostics.
  • Accurate characterization and prediction of complex aircraft engine degradation patterns.
  • Validation using NASA's C-MAPSS run-to-failure dataset.

Conclusions:

  • The proposed approach offers a robust solution for aircraft engine prognostics.
  • Effective sensor selection and adaptive modeling significantly improve prediction accuracy.
  • This method contributes to enhanced aircraft safety and operational efficiency.