Hi,
I want to measure blades first flap mode displacement in ADAMS for control applications, Is there anybody knows how this is possible in ADAMS?
Looking at relevant markers in FAST2ADAMSStatements.xls
MARKER 10000K 10000K BladeKCS_M Pitch plate center of mass of blade K - FAST blade K coordinate system
MARKER 10000K+J 10000K+J BladeKSecJRef_M Blade K, section (element) J, reference axes (attached to pitch axis and aligned with local aerodynamic axis)
MARKER 10000K+1000+10J 10000K+J BladeKSecJAero_M Blade K, section (element) J, aerodynamic MARKER
MARKER 10000K+2000+J 10000K+J BladeKSecJGraphics_M Blade K, section (element) J, GRAPHICS MARKER
MARKER 10000K+3000+J 10000K+J BldKSecJToBldSecBelow_M Blade K, section (element) J, connection to the blade section (element) below
MARKER 10000K+4000 10000K PitchPlateKToBldSec01_M Pitch plate connection to innermost blade section (element) for blade K
MARKER 10000K+4000+J 10000*K+J BldKSecJToBldSecAbove_M Blade K, section (element) J, connection to the blade section (element) above
Which markers I should use?
What about tower-top first fore-aft mode deflection?
Regards,