journal article·2023-08-20Open access

Statistical Algorithms with Phase-Sensitive Detection for the Number of Hovers and S Turns in Aircraft Flights

Moli Chen, Xunkai Wei, Hao Wang, Zhenhe Jiang

Applied Sciences· Volume 13· Issue 16

Abstract

Compared to maximum state parameters, such as maximum altitude and Mach, the number of hovers and S turns can be used as process parameters representing the complexity of military aircraft maneuvers when classifying big flight mission data to compile flight load spectra for structures. This study developed intelligent statistical algorithms based on yaw angle data from flight parameters such as the number of hovers and S turns. Using the median-crossing de-redundant function of Phase-Sensitive Detection (PSD) and analyzing the characteristics of 360° hovering flight parameters, a statistical algorithm for the number of hovers during a flight profile is presented. Using the split-half function of PSD, a triangle layering algorithm based on the yaw angle signal was developed to count the number of S turns during a flight profile, where the signal of each sublayer is segmented into median-crossing intervals to eliminate the redundant median-crossing marks from the previous layer. Compared with artificial means, the statistical results of the flight example showed that the developed intelligent algorithms are effective.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Structural Health Monitoring Techniques · Sensor Technology and Measurement Systems · Inertial Sensor and Navigation

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Beijing Aeronautical Engineering Technology Research Center, Beijing 100076, China

College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Funding

National Science and Technology Major Project

References (18)

Show source-provided references
1. Dynamic behavior analysis of intermediate bearing-squeeze film dampers-rotor system under constant maneuvering overload10.1155/2021/5512409 ↗
2. Coupled Lateral and torsional vibration of rub-impact rotor during hovering flight10.1155/2021/4077556 ↗
3. Breitkopf, G.E. (1989). Basic Approach in the Development of TURBISTAN, a Loading Standard for Fighter Aircraft Engine Disks: 19428-2959, ASTM International.10.1520/STP10349S ↗
4. Mission segment division of the whole aeroengine loading spectrum based on flight actions10.1016/j.cja.2021.06.015 ↗
5. Du, Y. (2018). Research on Aeroengine Load Spectrum Clustering Analysis Method and Simulation, Nanjing University of Aeronautics and Astronautics. (In Chinese).
6. A novel compilation method of comprehensive mission spectrum of aero-engine maneuvering load based on use-related mission segment10.1016/j.cja.2022.09.016 ↗
7. AirmanTesting Standards Branch (2023, April 15). FAA-H-8083-25: Pilot’s Handbook of Aeronautics Knowledge, Available online: https://www.faa.gov/pilots.
8. (1998). Joint Service Specification Guide, Aircraft Structures. Standard No. JSSG-2006.
9. Research on Generating Method for Severe Load Spectrum based on Individual Airplane Statistical Analysis
10. Generating methods of severe load spectra for airplanes based on statistic analysis flight subjects
11. Review and application of Rainflow residue processing techniques for accurate fatigue damage estimation10.1016/j.ijfatigue.2015.10.007 ↗
12. Highly Accurate Time-of-Flight Measurement Technique Based on Phase-Correlation for Ultrasonic Ranging10.1109/JSEN.2016.2631244 ↗
13. Dai, S., Nie, Z., Dai, H., and Chen, Q. (2018, January 10–12). Empirical mode decomposition based preprocessing of navigation data from flight data recording system. Proceedings of the 2018 IEEE CSAA Guidance, Navigation and Control Conference (GNCC), Xiamen, China.
14. Simulation of use-related multi-parameter load spectrum based on principal component analysis
15. Allen, M.J., and Dibley, R.P. (2003). Modeling Aircraft Wing Loads from Flight Data Using Neural Networks.10.4271/2003-01-3025 ↗
16. Neural networks modelling for aircraft flight guidance dynamics10.5028/jatm.2012.04020712 ↗
17. A multi-channel data-based fault diagnosis method integrating deep learning strategy for aircraft sensor system
18. Floris, H., Treve, V., Richard, C., and Visser, H.G. (2016, January 20–24). Evaluation of feasible machine learning techniques for predicting the time to fly and aircraft speed profile on final approach: Predictive dynamic support tool on final approach. Proceedings of the 7th International Conference on Research in Air Transportation, Philadelphia, PA, USA.