Aeroelastic effects on the B-2 maneuver response

Aeroelastic effects on the B-2 maneuver response

The Rodden-Love concept of correction for axes rotation is extended to the sensor-output equations, which are required for modeling of aeroservoelastic effects. Longitudinal maneuver analyses are performed and correlated with flight test data using the modified equations.

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Veröffentlicht in:Journal of aircraft 1995-07, Vol.32 (4), p.862-867
Hauptverfasser: Winther, B. A, Hagemeyer, D. A, Britt, R. T, Roden, W. P
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft
Applied sciences
Exact sciences and technology
Ground, air and sea transportation, marine construction
Mathematical models
Miscellaneous transportation
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Beschreibung
Zusammenfassung:The Rodden-Love concept of correction for axes rotation is extended to the sensor-output equations, which are required for modeling of aeroservoelastic effects. Longitudinal maneuver analyses are performed and correlated with flight test data using the modified equations.
ISSN:0021-8669
1533-3868
DOI:10.2514/3.46802