Load limiting control design for rotating blade root pitch link load using higher harmonic LTI models

Simple item page
dc.contributor.authorMballo, C.E.
dc.contributor.authorPrasad, J.V.R.
dc.date.accessioned2021-03-04T15:52:38Z
dc.date.available2021-03-04T15:52:38Z
dc.date.issued2018
dc.description.abstractThis paper discusses the synthesis of a load limiting controller (LLC) for critical helicopter components that are subjected to significant fatigue loading. The development of a (structural) load limit violation detection and limit protection algorithm using a linear time invariant (LTI) model of helicopter coupled body/rotor/inflow dynamics is described. The developed load limiting controller is evaluated in its ability to limit harmonic pitch link loads and its impact on maneuver performance for a typical longitudinal doublet input.
dc.identifier.other68 - Load limiting control design for rotating blade root pitch link load using higher harmonic LTI models.pdf
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3973
dc.language.isoen
dc.titleLoad limiting control design for rotating blade root pitch link load using higher harmonic LTI models

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
68_ERF_2018.pdf
Size:
842.82 KB
Format:
Adobe Portable Document Format
Download

Collections

Papers