Matched Filter Concept and Maximum Gust Loads

Matched Filter Concept and Maximum Gust Loads

In the course of NASA evaluations of the statistical discrete gust method for determining worst-case gust loads on aircraft, it was found that the concept of the matched filter from signal processing theory could be applied to the analysis of time-correlated, worst-case gust loads for mathematically...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of aircraft 1997-01, Vol.34 (1), p.101-108
1. Verfasser: Zeiler, Thomas A
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Aircraft
Applied sciences
Exact sciences and technology
Ground, air and sea transportation, marine construction
Mathematical models
Miscellaneous transportation
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:In the course of NASA evaluations of the statistical discrete gust method for determining worst-case gust loads on aircraft, it was found that the concept of the matched filter from signal processing theory could be applied to the analysis of time-correlated, worst-case gust loads for mathematically linear aircraft models.
ISSN:0021-8669
1533-3868
DOI:10.2514/2.2141