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Add Mean_PtfmPitch to openmdao outputs #102

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Merged
dzalkind merged 1 commit into from
Apr 16, 2026
+4 −2
Merged

Add Mean_PtfmPitch to openmdao outputs #102

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6 changes: 4 additions & 2 deletions raft/omdao_raft.py
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Original file line number Diff line number Diff line change
Expand Up @@ -322,8 +322,9 @@ def setup(self):
# Aggregate outputs
self.add_output('Max_Offset', val = 0, desc = 'Maximum distance in surge/sway direction', units = 'm')
self.add_output('heave_avg', val = 0, desc = 'Average heave over all cases', units = 'm')
self.add_output('Max_PtfmPitch', val = 0, desc = 'Maximum platform pitch over all cases', units = 'deg')
self.add_output('Std_PtfmPitch', val = 0, desc = 'Average platform pitch std. over all cases', units = 'deg')
self.add_output('Max_PtfmPitch', val = 0, desc = 'Maximum platform pitch over all cases', units = 'deg')
self.add_output('Mean_PtfmPitch', val = 0, desc = 'Maximum mean platform pitch over all cases', units = 'deg')
self.add_output('Std_PtfmPitch', val = 0, desc = 'Average platform pitch std. over all cases', units = 'deg')
self.add_output('max_nac_accel', val = 0, desc = 'Maximum nacelle accelleration over all cases', units = 'm/s**2')
self.add_output('rotor_overspeed', val = 0, desc = 'Fraction above rated rotor speed')
self.add_output('max_tower_base', val = 0, desc = 'Maximum tower base moment over all cases', units = 'N*m')
Expand Down Expand Up @@ -870,6 +871,7 @@ def compute(self, inputs, outputs, discrete_inputs, discrete_outputs):
outputs['Max_Offset'] = np.sqrt(outputs['stats_surge_max'][case_mask]**2 + outputs['stats_sway_max'][case_mask]**2).max()
outputs['heave_avg'] = outputs['stats_heave_avg'][case_mask].mean()
outputs['Max_PtfmPitch'] = outputs['stats_pitch_max'][case_mask].max()
outputs['Mean_PtfmPitch'] = outputs['stats_pitch_avg'][case_mask].max()
outputs['Std_PtfmPitch'] = outputs['stats_pitch_std'][case_mask].mean()
outputs['max_nac_accel'] = outputs['stats_AxRNA_max'][case_mask].max()
outputs['rotor_overspeed'] = (outputs['stats_omega_max'][case_mask].max() - inputs['rated_rotor_speed']) / inputs['rated_rotor_speed']
Expand Down
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