1 Introduction
First concept and feasibility studies for fowt appeared more than 15 years ago Henderson2000 . Since then, prototypes of spars, semisubmersibles, barges and tlp have been built Tande2015 . The present paper aims at particular design indicators for semisubmersibles for a favorable response behavior in wind and waves. The next sections will first provide an introduction of the inherent fowt dynamic characteristics followed by a review of published design procedures.
1.1 System dynamics of floating wind turbines
The commonly employed dynamic aerohydroelastic models for fowt involve assumptions comparable to the FAST model by nrel FAST8
. This opensource tool is used as a reference model in the present work.
Most models employ elastic mbs of reduced order through an approximation of the tower and blade deformation with a superposition of their respective mode shapes. FAST has in this work 25 enabled dof. The loworder model, on the other hand, has six dof, covering only the 2D planar motion of the system. The term “loworder” refers in this work to the number of dof of the dynamic equations of motion. Coupled dynamic models consider, next to the elastic forces, centrifugal, gyroscopic and Coriolis forces, which are significant for systems of large rigidbody motions. The coupling effects are important for the system dynamics, because the elastic body mode shapes vary when coupled into a multibody system. An example is the coupling of the tower flexibility with the floater rigid body modes or the controller closedloop dynamics with the foreaft mode.
The wind turbine blade pitch controller is especially critical for fowt: A standard rotorspeed controller for aboverated wind speeds will pitch the blades when the rotor speed exceeds its rated value. In the case of fowt, this feedback loop can imply, as a sideeffect, that the tower or the platform experiences large excursions, due to the aerodynamic properties of the rotor. When the relative wind speed (the one seen by the rotor) increases, the controller will pitch the blades towards feather (increasing blade pitch angle) and thereby reduce the aerodynamic rotor torque. As a consequence, the thrust also decreases. This means, on the other hand, that an oscillation of the platform in pitch will become unstable if the controller reacts sufficiently fast to the sinusoidally oscillating relative wind speed, see Jonkman2008 ; Larsen2007 .
External excitations arise from wind and waves. The wind turbulence excites the lowfrequency platform modes as well as the blades and the towertop at multiples of the rotor rotational frequencies. Dynamic effects due to the foreaft motion of the rotor, accelerating the bulk flow across the turbine are subject to current research, i.e. Hansen2014 ; Tran2015 ; Lennie2017 . Hydrodynamic forces, important for the system dynamics of semisubmersibles, are the FroudeKrylov wave loads including diffraction, viscous drag excitation, viscous drag damping (both from Morison’s drag term) Matha2019a ; Massie2001 ; mccormick2010 and secondorder slowdrift forces at the differencefrequency of bichromatic waves from potential flow theory, i.e. Faltinsen1993 ; Duarte2014 . The firstorder wave force coefficient can feature an attenuation range for semisubmersibles, also called the “wave cancellation effect”, see Hanna1986 and (Patel1989, , p. 290). For a representation of the overall fowt response, the mooring line dynamics might be of negligible influence in the case of catenary mooring lines Azcona2016a ; Matha2016a .
1.2 Floating wind turbine design
Several schemes for the sequential design of fowt have been published in Huijs2013 ; Azcona2013 ; Fernandez ; Crozier2011 ; Liu2018 . The report of the European project LIFES50+^{2}^{2}2http://www.lifes50plus.eu, accessed on July 18, 2018. Muller2015 provides a comprehensive literature review of the fowt design process and summarizes the findings in a consolidated scheme consisting of three stages. This work does not introduce a new design procedure, but a favorable effect that becomes visible in an integrated simulation study, covering a range of system parameters. In order to understand the existing constraints and barriers for an integrated design procedure, these are outlined in this section, before addressing the present design and simulation methodology.
Commonly, the design of a floating platform starts with static calculations, the socalled spreadsheet design phase. In this phase, the main dimensions of the structure can be determined, satisfying the requirement of hydrostatic restoring with an approximate structural dimensioning. It includes also frequencydomain analyses of the floater rigid body and the mooring lines. The first stage terminates with first experiments and an approximation of the expected cost of energy. In the subsequent stage, the first coupled dynamic simulations take place, which require a wind turbine model and a controller.
The manifold of design constraints of a fowt are represented in various standards and guidelines Atcheson2016 . Published design studies have addressed the structural integrity, dynamic behavior, manufacturing, installation and marine operations, among others. An academic concept design study across different platform types was presented in Lefebvre2012 , outlining the main assumptions and design constraints. A spar platform out of concrete was designed, simulated and tested in Molins2014a ; Matha2015 . The constraints and options for manufacturing of that design are discussed and summarized in Molins2018 . A comparable design of reduced draft was presented in DeGuzman2018 with a focus on seakeeping of the floater and marine operations. The peculiar loads of a steel semisubmersible with submerged counterweight are calculated in Pereyra2018 with a focus on the cables, sustaining the counterweight. A semisubmersible for a very large wind turbine was recently presented in Liu2018 .
Further studies focused on methods for obtaining the structural stresses of the floater in extreme and fatigue load cases. One of the first approaches was presented for a steel semisubmersible in Aubault2009 . The difficulty of obtaining the structural loads is due to the fact that most available coupled simulation codes assume the floater is rigid, which makes it impossible to calculate internal stresses. Ways to overcome this limitation were presented in Luan2013 ; Luan2017 ; Borg2017 ; Nygaard2015
. These methods involve either additional dof of the dynamic model or additional engineering steps in decoupled analyses. Often, the towerbase bending moment, which is available in standard simulation models, is taken as representative structural load in optimization studies. It is influenced by both, wind and wave loads.
First integrated optimization studies for tlp and spars were presented in Sclavounos2007 . A coupled frequencydomain model was used to calculate the towertop acceleration for various shapes of the floating platform and different slack and taught mooring configurations. Later, optimization studies on spar platforms were presented Fylling2011 , including load calculations and a cost model. An adaptation of the wind turbine controller was first included using the same simulation model as in the present work in Sandner2014 ; Lemmer2017 .
A large optimization study across different platform types was published in Hall2013 and later extended in Karimi2018 . It includes the hull shape and mooring line design and a genetic optimizer. In that work, a frequencydomain model is derived from the code FAST FAST8
, with a linear representation of the hydrodynamic viscous damping but without representing the wind turbine controller. The objective was also here a low nacelle acceleration, next to the estimated cost. The objective of the present work, as well as the design and simulation methodology will be outlined in the next section.
1.3 Parametric design and simulation approach
The methodology of the present work builds on parametric design routines (i.e. estimating steel thicknesses for structural integrity) on the one hand and parametric simulation models on the other hand. The design task in this paper considers a variation of the hull shape of a threecolumn concrete semisubmersible with varying draft and the wind turbine controller.
Figure 1 shows the main steps: The initial free variables parameterize the hull shape. As a function of these, a reasonable design space will be defined, with only few free variables to clearly visualize, interpret and understand the results, as shown in the next section. Based on this initial design space, the spreadsheet design routines ensure that each design satisfies basic constraints, related to the structural dimensions and the hydrostatic restoring, which is subject of Section 3. The result of this step is a design space of only two dimensions. The designs range from a slender, deepdrafted semisubmersible to a design of large breadth, large column radius and shallow draft. All designs are threecolumn semisubmersibles with heave plates. Hence, no discontinuities are present.
An adapted loworder aerohydroservoelastic simulation model will be used for the analysis, as introduced in Section 4. It includes all effects relevant for the main system dynamics, which are sought to be optimized. Therefore, effects like the floater structural elasticity or advanced aerodynamic effects are not considered. For all shapes, the firstorder hydrodynamic coefficients are calculated through a parameterized panel code model. These coefficients are input to the loworder model. The model includes Newman’s approximation to account for secondorder slowdrift forcing. It includes also memberbased viscous drag coefficients. The model is described in detail in Lemmer2018e ; Lemmer2018a .
The viscous heave plate drag model is rather detailed because it influences the foreaft motion and the coupling with the controller. The vertical heave plate drag coefficients are parameterized as a function of the KeuleganCarpenter number , which depends on the significant member length , the response velocity magnitude and its period .
The wind turbine bladepitch controller design routine is a function of a linear statespace model, including the viscous drag coefficients. For this reason, the system response has to be solved for iteratively because the controller depends on the drag coefficients, which in turn depend on the response magnitude. Examples for the analyzed results of Section 5 are the fatigue and extreme loads under realistic loading conditions, the modal properties and the harmonic response behavior to wind and waves.
The results of Section 6 will analyze and visualize the distinct dynamic properties across the design space. This analysis helps to understand the effects, which drive load and power fluctuations. From the findings, a new design objective is derived, extending the one of the nacelle acceleration used in previous works. The objective is focused on the dynamic system response while the component design is out of the scope of this paper.
2 Design Space
The selected hull shape parameters include the column spacing from the platform centerline , the column radius , the heave plate height , the ratio of heave plate radius to column radius and the draft , see Figure 2.
The column radius is defined to be of the maximum possible column radius at which the three columns would touch each other. The heave platetocolumn radius ratio is intended to be for all designs in order to ensure that the heave plates are large enough to effectively alter vertical added mass and FroudeKrylov forces. The heave platetocolumn radius ratio is altered, however, for the designs where the heave plates of the different columns would get too close to each other through an exponential function
(1) 
This ensures that no designs with unrealistically large heave plates result, which might not be manufacturable. The distance between overall center of mass and metacenter , i.e. mccormick2010 , determines the restoring as
(2) 
with the displaced volume of density and the gravity constant . Ballasting is such that zero trim is achieved. Thus, for given column diameters, a required can be obtained by increasing the draft , which lowers the center of gravity more than it raises the center of buoyancy and therefore increases .
An upper draft limit of was considered in the apriori definition of the bounds of the free variables. Hence, any shape considered in this study can be described by the two free variables column spacing and heave plate height . This means that the design space (of the free variables) is Cartesian and the range of every variable does not depend on the values of the others. The small design space of feasible platforms makes a visualization and thorough analysis of the results possible. Table 1 lists the free variables and the dependent variables.
Free variables  Dependent variables 

• Column spacing  • Column radius 
• Heave plate height  • Heave plate radius 
• Draft  
• Steel tripod strut width &  
sheet thickness  
• Ballast mass  
• Platform mass distribution  
• Mooring line fairleads position  
• Wind turbine controller gains 
The semisubmersible main dimensions of the 2D design space are shown in Figure 3 with a column spacing range and a heave plate height range . The designs range from slender, rather ballaststabilized towards buoyancystabilized shallowdrafted semisubmersibles. Larger column spacings than the ones considered are expected to result in excessive bending stresses in the tripod structure. The variable heave plate height has the main effect of modifying the vertical FroudeKrylov forcing. Thus, this variable may be able to facilitate the abovementioned wave cancellation effect. The images on top of Figure 3 show that the column radius is largest for the lowest draft. The cost increases generally for increasing column radii but decreases for the buoyancystabilized ones of shallow draft. The assumptions for the material cost estimation will be given in Section 3, it is roughly proportional to the submerged volume. The three designs shown in Figure 3 will be selected in a number of the upcoming analyses and indicated by “deep draft”, “medium draft”, and “shallow draft”.
3 Parametric Design Routines
This section addresses the design routines, which determine the dependent variables of Table 1. It starts with the structural design of the concrete floater with the steel tripod on top, followed by the mooring lines and the tower. Hydrostatic computations and the panel code calculations follow thereafter in Sections 3.2–3.3. The wind turbine controller is also parameterized and subject of Section 3.4. The wind turbine design, used for all platforms, is the DTU rwt of Bak .
3.1 Structural design
Design routines, which were developed for the concrete columns, the heave plates and the steel tripod will be described in this section. The result of the structural design calculation is mainly the mass distribution, next to the shape of the hull, which will be input to the coupled simulation model. The assumed material properties, costs and wall thicknesses of the columns are listed in Table 2, based on Lemmer2016a .
Parameter  Unit  Value 

Reinforced concrete average density  []  2750.0 
Steel density  []  7750.0 
Ballast density  []  2500.0 
Processed steel cost  []  4500 
Processed concrete cost  []  399 
Concrete column wall thickness  [m]  0.6 
Heave plate upper and lower lid thickness  [m]  0.4 
3.1.1 Steel tripod
For the steel tripod, various fe analyses were performed, covering the range of radial distances of the columns as shown in Figure 3. The results of these calculations allow a parameterization of the dimensions of the steel legs like the sheet metal thickness, the strut width and height. The calculations assume a static thrust force at the towertop of , as given in (Bak, , p. 61). The notch stress at the joint between the tower and the tripod struts is assumed to be the critical failure mode. The dimensions of the struts are determined such that the maximum notch stress is of comparable magnitude as the one resulting from the same calculation with a comparable commercial tripile. The method was first applied in the European project INNWIND.EU^{3}^{3}3http://www.innwind.eu, accessed on July 18, 2018., of which details can be found in innwindd433 . The dimensions of the tripod of the minimum and maximum column spacing are shown in Table 3.
Min. column spacing  Max. column spacing  
Column spacing  
(distance to center)  
Strut width & height  
Steel wall thickness  
Maximum stress  
Tripod mass 
3.1.2 Concrete columns and heave plates
The concrete columns are of prestressed concrete following the example of the AFOSP spar design, see Molins2014a . The cylindric walls have a constant thickness for all of the hull shape variations, see Table 2. The heave plates are made out of reinforced concrete with the material properties given in Table 2. The heave plates are concrete rings, flush mounted to the lower ends of the columns. This assumption is rather conservative and accounts for further compartmentation and reinforcements of the detailed design phase.
3.1.3 Mooring lines
The properties of the mooring system can be found in Lemmer2016a . It was designed for the TripleSpar design Lemmer2016a ; Bredmose2017 , with two upwind lines and one downwind line with fairleads above swl, at and a radial distance from the tower centerline of . This large distance makes it possible to keep the same mooring system for all column spacings of Figure 3.
3.1.4 Tower
The tower design is not varied in the optimization study but the parameters of the reference TripleSpar are used Lemmer2016a . For fowt it is important that the tower eigenfrequency does not coincide with the 3pfrequency range of the rotor. However, the considered platforms of Figure 3 show only little variations of the eigenfrequencies. This is mainly due to the hydrostatic design constraints (Section 3.2). Consequently, no adaptation of the tower design is considered in this work.
3.1.5 Cost estimation
fowt cost models have been subject of different research projects with a good overview and summary in Benveniste2015 ; Lerch2018 . For this work, a cost of the processed material of the concrete heave plates and columns and the steel tripod, including both, material and manufacturing costs, is assumed. The values are in line with LIFES50+ Deliverable 4.3 Lemmer2016d and can be found in Table 2. The cost levels shown in Figure 3 are comparable to the ones of Lerch2018 . Other costs than the ones mentioned, like installation, assembly and O&M costs are not considered. It is noted that these values are rough approximations, which might change due to concrete shrinkage and also due to existing price fluctuations over time.
3.2 Hydrostatic design
The hydrostatic restoring stiffness in pitchdirection is a driving property, which influences the fowt mean pitch angle under wind loads and therefore the power losses from misalignment, the maximum amplitudes and the eigenfrequencies. In other works, such as Hall2013 , the value of is free to vary in the design space and constraints on the pitch eigenfrequency are imposed.
In this work, the hydrostatic restoring was constrained, following the perception that the hydrostatic restoring is crucial for the abovementioned fowt properties. A variation of might result in small changes in cost and performance, while a large change of its value is unrealistic. The restoring is set as constraint for all geometries of the design space. Depending on the free variables column spacing and heave plate height , the draft, as remaining variable, is determined such that this constraint is satisfied. A rootfinding algorithm, connected to the structural design and the hydrostatic functions, solves this problem. The steady state pitch angle is about at rated wind speed. It would change as a function of the fairlead vertical position, due to a different lever arm of the rotor thrust force. This vertical position, however, is constant throughout the design space.
3.3 Hydrodynamic coefficients
A parameterized panel model has been set up to calculate the hydrodynamic coefficients with Ansys AqwaLine.
The column drag coefficient is kept constant for all designs and seastates. It has been selected conservatively as . In the case of the heave plates, the drag coefficient is iterated based on the experimental data given in Tao2008 . This data was parameterized as a function of , which is possible because the Reynolds number and the surface roughness have little influence for shapes of sharp edges. For all designs, the vertical drag force is applied only at the lower (keel) surface of the heave plates and the bottom crosssectional area of the heave plates is used for the calculation of the drag force. The iterative procedure is subject of the paper Lemmer2018c .
3.4 Controller design
As introduced in Section 1, the blade pitch controller of the wind turbine for aboverated wind speeds is critical for the fowt system stability. In order to ensure a properly tuned controller for each of the designs of Figure 3, a method was developed to automate the design of a siso picontroller, depending on the linear dynamic model. This model will be introduced in Section 4. The controller design procedure is subject of the companion paper Lemmer2018d and part of the thesis Lemmer2018a , which includes a comparison against a multivariable controller.
Figure 1 of Section 1 shows on the right the iterative solution procedure to obtain the controller gains: It follows from the implementation of Lemmer2018c , which considers viscous drag coefficients of the heave plates that are a function of the number, which is itself a function of the nodal response magnitude. The resulting platform viscous damping eventually determines how aggressive the wind turbine controller can be tuned. Thus, the viscous drag and the blade pitch controller gains are obtained iteratively.
The parameterized control design routine has proven to be valid throughout the entire design space of platforms, which was verified through simulations over all operating wind speeds. Especially the rotor speed and power overshoots are for all platforms within the design space and the metocean conditions of (Krieger2016, , Chap. 7) inside commonly used design constraints.
4 Simulation Model
The numerical fowt model used for the computation of the load response in this work was described in Lemmer2018a ; Lemmer2018e . Figure 4 shows a mechanical sketch of the slow model. The intended purpose of the model is to represent the overall rigidbody and elastic dynamics of the system. It shall, on the other side, disregard all effects which increase complexity without contributing to the main system response. Through the improvement of computational speed, an efficient calculation of the load response for all designs is possible. The model derivation starts with physical (as opposed to blackbox) models, keeping the inherent nonlinearities. Subsequently, these models are linearized and the frequencydomain response spectra will be used here, which is subject of Section 5.
The structural model is derived using the theory of flexible mbs. An advantage of the implemented algorithm is that the setup of the equations of motion is userdefined. Thus, the multibody structure can be adapted to the analyzed problem. In this work, the equations of motion have been set up for six dof in 2D: The floating platform rigid body in surge (), heave () and pitch (), a flexible tower with one generalized coordinate , the rotor speed and the blade pitch actuator is selected, see Figure 4. These dof are chosen with the aim of reducing the system to the most important forces and response dynamics. The largest environmental forces act usually in the direction of wind and waves ().
The aerodynamic model avoids an iterative solution of the lift and drag forces on the blade sections Hansen2000 . Instead, the bulk flow across the entire rotor is considered and the rotor thrust and torque is calculated as function of the tsr and the blade pitch angle, using the rotor thrust and power coefficient. This method neglects azimuthdependent forcing, especially through wind shears. These are reintroduced through a rotational sampling of turbulence at the rotor rotational frequency. The method has proven to be a good tradeoff between accuracy and efficiency, especially for the optimization of the fowt substructure, as shown in Lemmer2018a .
The hydrodynamic model uses the firstorder panel code coefficients and a nodebased Morison drag model for a reliable representation of the foreaft viscous damping, as introduced in Section 1. A significant improvement of the computational efficiency is achieved through the frequencyindependent added mass and the neglected radiation damping. It is shown in Lemmer2018a that radiation damping is of little influence for the considered platforms, because the dominant forces at the frequencies of nonzero radiation damping are the firstorder wave forces. Newman’s approximation Standing1986 is employed to account for lowfrequency slowdrift forcing. The mooring forces result from a quasistatic model.
The nonlinear equations of motion are linearized about all operating points, resulting in a linear statespace description. The aerodynamics are linearized with a tangent approximation of the rotor coefficients through a central difference scheme. The quadratic drag is linearized through Borgman’s method Borgman1965a , using the std of the platform nodes, obtained from an iterative frequencydomain solution. The linear model is only valid for small deviations of the states from the operating point. For this reason, the analyzed results focus on operational rather than extreme load cases. To prove the validity of the results, Section 5 will include a comparison against the higherfidelity FAST model.
5 Load Calculation
This section presents the results of load calculations in operational conditions across the design space. First, selected signal statistics will be compared, weighted with the probability of occurrence of each environmental condition over a lifetime of 20 years in the same way as Smilden2017 . Thereafter, the frequencydomain response will be analyzed and the results will be verified through a comparison against the reference model FAST. A design indicator will be presented at the end of this section, which is able to predict the optimal response behavior.
The environmental conditions of the project LIFES50+ are used with a significant wave height up to , see Table 4. For each wind speed, three different peak spectral periods are considered, each with a probability of occurrence of 1/3 for the respective mean wind speed. Onehour simulations are performed with both timedomain models, cutting the transient for statistical evaluation.
Wind speed  5.0  7.1  10.3  13.9  17.9  22.1  25 

Significant wave  1.4  1.7  2.2  3.0  4.3  6.2  8.3 
height  
Peak spectral  5.0  5.0  5.0  7.0  7.5  10.0  10.0 
period  
7.0  8.0  8.0  9.5  10.0  12.5  12.0  
11.0  11.0  11.0  12.0  13.0  15.0  14.0  
Probability [%]  14.8  25.0  28.7  17.5  5.9  0.9  0.1 
5.1 Operational load response
The linear frequencydomain SLOW model of Section 4 is used to simulate the response to the metocean conditions of Table 4 for thirty platform designs of the parameter space of Figure 3.
Figure 5 shows the statistical results of the IEC dlc 1.2 IEC2007 , weighted with the Weibull probability density function of Table 4. The del of the towerbase foreaft bending moment is calculated for a lifetime of 20 years with a Wöhler exponent of . The std are normalized with the corresponding values for the onshore DTU rwt with the same turbulent wind fields. For onshore turbines, the significant loading through the waves is not present and only the harmonic loads of the 1p and 3pfrequencies are the main fatigue drivers. It can be seen that the weighted del of has a minimum at the shallowdraft shape (, ). The same holds for the weighted std of the rotor speed (which is proportional to the power for aboverated winds) and the platform pitch angle (here the minimum is at the thinnest heave plate ). The blade pitch activity () is rather constant over the design space.
These results show a towerbase bending damage variation of more than . The fatigue damage is for the optimal design only greater than for the onshore turbine, although the wave conditions are rather severe. The estimated material cost of this design is not significantly higher than the one of the deeper draft, see Figure 3, although the shallowdraft platform has a large column spacing of and a column radius of with heave plates of .
Figure 6 shows a comparison of the response spectra of the deepdraft and the shallowdraft platforms. The shallowdraft shape has a larger differencefrequency and windinduced response in surge at the lower end of the frequency axis. Except for this, the reason for the good performance, indicated by Figure 5, becomes clear: The shallowdraft platform has visibly smaller responses at the pitch eigenfrequency of but, even more importantly, at the firstorder wave frequencies of (, left) and (, right). This effect is noticeable for the platform motion response but even more for the tower bending (, ), the rotor speed and the electrical power .
5.2 Comparison of design model and reference model
Figure 7 shows the same response signals as Figure 5 with a comparison between the nonlinear and the linearized slow models and the FAST model. The comparison shows the results of all column spacings for the flattest heave plate and the thickest heave plate . The qualitative optimum towards large (shallow drafts) is predicted equally by all models. Consequently, the loworder model is generally suitable for the considered conditions and assessed response quantities.
There is a constant conceptindependent offset of the del between the slow models and FAST. The reason for this offset is the simplified actuator disk model. The excitation of the blades through wind shear is only reintroduced through a rotational sampling of the bladeeffective wind at the nominal rotor speed, see Lemmer2018e . The offset of the rotor speed and blade pitch angle is related to the linearized slow model. The linearized model underpredicts the variation of the rotor responses because of the nonlinear switching algorithm of the controller. The objective of the belowrated controller is to maximize power production, while the aboverated controller aims at limiting the power production. The switching between the control regions is a highly nonlinear effect, which cannot be modeled with the linear frequencydomain model. It is, however, modeled in the timedomain model, which agrees notably better with FAST for and . The platform pitch angle variation is well aligned among the timedomain models with a slight underprediction of slow for the platforms of deep draft. The linearized model underpredicts the pitchstd for the shallowdraft platforms. This effect is distinct for the two heave plate heights and might therefore be due to the simplified radiation model, see Lemmer2018e .
5.3 Extreme load response
The load response to IEC dlc 6.1 with 50year wind and wave conditions is presented in this section. The reference model FAST was used in this case because of large expected excursions, where especially the aerodynamic model of slow might not predict reliable results, due to its simplifications. Turbulent wind and irregular wave timeseries were generated according to (Krieger2016, , p. 58, 64). Figure 8 shows the mean of the maxima of the towerbase bending moment and the towertop acceleration (the absolute one, including platform accelerations) of three onehour simulations. The results confirm the findings of Figure 5: The shallowdraft platform has small towertop accelerations of less than . The LIFES50+ design basis Ramachandran2017 would accept these values even during operation, while the limits for shutdown conditions are .
6 Results Analysis and Design Indicators
A key to understanding the underlying effect for this remarkable ability of the shallowdraft platform () to reject disturbances is the analysis how the system responds to sinusoidal disturbances, meaning regular waves of different frequencies or harmonically oscillating wind speed. The ability to reject these disturbances will be quantified with a new design indicator at the end of this section.
6.1 Harmonic response to wind and waves
Figure 9 shows the harmonic response to wind and wave forces. The lines, representing each a different frequency, stand for the fowt centerline response. The horizontal distance of each point on the lines to the axis indicates the amplitude of oscillation of the system response at all elevations along the centerline to sinusoidal wind (upper) and wave excitations (lower). The analysis is made with the loworder linearized model of Section 4 with firstorder hydrodynamics, quasistatic mooring lines, an elastic tower, aerodynamics and the tuned picontroller at . The centerline amplitude results from the disturbance transfer function or rao from wind () and waves () to the states surge, pitch and towerbending, represented by as
(3) 
The tower shape function is denoted by .
The solid black horizontal lines indicate the overall cm of the fowt and the dashed line indicates the center of buoyancy. For ships, the instantaneous center of roll motions is usually the metacenter, (Fossen2011, , p. 62). Here, the instantaneous center of rotation in pitch is the vertical location on the platform with nearzero amplitude. The response to harmonic wind excitations shows a center of rotation equal to the cm. The same behavior is generally observable for all platforms.
The lower part of Figure 9 shows the harmonic response to waves. Here, the instantaneous center of rotation is below the platformcm for the platforms of deep draft. The platform of the lowest draft () has a different behavior: Its instantaneous center of rotation is at higher elevations, near the rotor hub. This is remarkable because it means that the hub does not respond with a horizontal movement to wave excitations. Consequently, the wind turbine power production is almost not affected by the waves and the rotor does not see any platforminduced relative wind speed. The shallowdraft platform responds in a way that surge is positive, when pitch is negative. Thus, these dof are outofphase, as opposed to the other platforms, which have an inphase response of surge and pitch to waves. Therefore, this optimality cannot be found when the surge or pitch rao is sought to be minimized. The same idea inspired the developers of a tlp platform to arrange the taut mooring lines, such that the system is forced to rotate about the hub, see Melis2016 . The fact that this behavior can be obtained for semisubmersibles has not been published yet.
The cause leading to this response behavior are the FroudeKrylov pressures, integrated over the hull surface. The coupled magnitude and phases of the forcerao vector
are for the optimal shape such that the presented response of the fowt system is obtained. Semisubmersibles are predestined for a “shaping” of the forcerao because the floater members see different phases of the waves and, additionally, the horizontal (heave plates) and vertical (columns) surfaces experience different phases of the FroudeKrylov pressures, which allow a counterphase surge and pitch forcing.Eventually, the shallowdraft platform motion is not constrained but a motion response to mitigate the wave pressures is allowed. Important is the fact that the allowed motion response is favorable, such that the transmissibility of the wave forcing towards the wind turbine is reduced. The smaller towertop motion yields smaller inertial forces of the rna. The bending moments from the gravitational forces of the rna are reduced because the platform pitch angle is also smaller for the shallowdraft design (Figure 5). The aerodynamic damping forces are not significant at the wave frequencies Lemmer . In conclusion, the stationary hub does not only yield a smooth power production but also reduced towerbase bending moments. Small adjustments in the optimal harmonic response shape can be expected when taking other outputs, like the mooring fatigue, into account.
The “counterphase pitch response” of Figure 9 is important for the controller design: Because of the minimal motion response at the hub, the power fluctuations are reduced. Also, the coupling of the substructure dynamics with the controller is reduced. Common controllers feed back the rotor speed deviation from the set point. If the rotor responds less to the wave forces, there will be less waveinduced rotor speed deviation and the wave response will not be amplified by the controller as with regular fowt platforms. It is emphasized that the harmonic response is not to be confused with the modal response to turbulence and slowdrift forces. This one can be well damped by wind turbine controllers, which feed back a foreaft velocity signal, as in Fleming2016 , Olondriz2017 or Yu2018 . It was shown in Fleming2016 ; Lemmer that the system response to firstorder waves cannot be damped by the controller because of their large magnitude. Consequently, the shaping of the hull which yields the favorable firstorder wave response can be effectively complemented by a controller, which damps the lowfrequency motion response.
The sensitivity of this behavior to the peak spectral wave period is obvious from Figure 9. Thus, the favorable design is sitedependent. It can be seen, however, that the sensitivity is not very pronounced, meaning that the instantaneous center of rotation does not move significantly as a function of the wave frequency. This shows a certain robustness of the response behavior in terms of the environmental conditions.
6.2 Design indicator: Minimum required control action
The harmonic response of Figure 9 helps to understand the reason for the favorable behavior of the shallowdraft platforms. In this section, a new design indicator will be introduced to generally judge the goodness of a platform in terms of its induced wind turbine response. The idea is to quantify the necessary controller action to perfectly cancel the external forcing from wind and waves. The smaller the controller activity, the better the capability of the design to inherently reject disturbances itself. Figure 10 shows the linear fowt system transfer function in the Laplace domain with additive disturbance transfer functions for the control inputs generator torque and blade pitch angle and the outputs rotor speed and towertop bending . Both, the plant and the disturbance transfer function for wind and the one for waves , collected in , are obtained from the linear slow model and scaled as in Lemmer . This is convenient as it means that a response exceeds the design limits, see Skogestad2005 .
In order to quantify the impact of disturbances on a linear system, Skogestad Skogestad1996 calculates the 2norm of the control input, theoretically necessary to perfectly cancel the disturbances. This analysis does not consider the controller dynamics but only the actuator authority on the system response. The required control input can be obtained, given a disturbance , through system inversion as
(4) 
The least necessary actuation^{4}^{4}4Calculated for both control inputs , assuming the most effective combination of them, through a svd of . is the 2norm of the control input vector. has been calculated for the different platforms for the wind excitation and wave excitation independently in Figure 11. The part from wind excitation (upper part of Figure 11) does not show a large variation over the different platforms, except for the changing eigenfrequencies. It is different for the wave excitation: The best performance (equal to the least required actuation ) results here for the largest column spacing . Consequently, the assessment of the minimum required control input can well predict the optimality of the semisubmersibles, seen in the Figure 5 and 9.
This indicator allows a general quantification of the ability of a fowt platform to support a wind turbine without transmitting detrimental external excitation forces. It is the basis for a platform design, particularly adapted to the requirements of the wind turbine.
Parameters of optimum design
A FAST model of the optimum shape can be downloaded Lemmer2018b . The hull shape has a column radius of , a spacing from the centerline of a heave plate thickness of a draft of . The platform has a mass including ballast of and a center of mass below swl of .
7 Conclusions
The study can be summarized by two parts:
First, an integrated optimization procedure for semisubmersible fowt was set up. A small design space of a threecolumn semisubmersible with heave plates was defined, ranging from a slender deepdrafted geometry to a shallowdraft one with large column diameter. A tailored coupled simulation model of low order was employed to calculate the system response, but also for the design of a wind turbine controller that is tuned for each platform design. As a result of the optimization, the design of lower draft gave a remarkable improvement of the response of the towerbase bending.
Second, a detailed analysis of the results revealed a particularly favorable response behavior to firstorder waves, which can be represented by a new design indicator. The identified optimum is mainly due to an efficient design of the hull shape, yielding a favorable response behavior: The harmonic response function, derived from a linearized loworder model, revealed the dynamic characteristics of the optimum shape. It shows almost no foreaft motion at the rotor hub, which means that the entire system, subject to wave loads, rotates about this point. As a result, the hub is almost stationary and the fluctuations of the power, the rotor speed, generator torque and blade pitch angle can be significantly reduced. An interpretation of this is that the surge and pitch response are outofphase, yielding a positive surge displacement when the pitch angle is negative.
In order to consider this optimal dynamic behavior of semisubmersibles in future design practices, a new performance indicator was developed: The “least required actuator action” is considered, the action of the blade pitch angle and generator torque. Their magnitude, necessary to reject the wave loads, is an indicator, which can effectively predict how well a floating platform is able to inherently reject disturbances itself, without transmitting them to the wind turbine.
The study showed that it is possible to design a fowt platform, specifically suitable to carry a wind turbine, minimizing the effect of the waves on the power production. While the firstorder wave loads cannot be mitigated by the controller, a further improvement of the lowfrequency response behavior through the controller is possible. The presented harmonic response graph can be a good means for the selection of additional feedback loops. Although the cost model of this work is simple, the work follows the idea that a smooth behavior in harsh metocean conditions is a key for a sustainable and lowcost fowt design.
Further studies will address the impact of the counterphase response on the mooring line loads and integrate them into an optimization process.
Acknowledgements
The research leading to these results has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No. 640741 (LIFES50+).
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