A novel control structure for wind turbine with synchronous generator for tower load reduction
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1 mme.modares.ac.ir * 2 2 imani@um.ac.ir *. () : : : A novel control structure for wind turbine with synchronous generator for tower load reduction Arash Hatami, Behnam MoetakefImani * Department of Mechanical Engineering, Ferdowsi University of Mashhad, Mashhad, Iran * P.O.B , Mashhad, Iran, imani@um.ac.ir ARTICLEINFORMATION ABSTRACT OriginalResearchPaper ReceivedJune26 Accepted24September26 Available Online 26 October 26 Keywords: Multivariable adaptive control Wind turbine simulator Mechanical load reduction Nonlinear model [2]. 66 The attenuation of mechanical load is one of the most effective approaches in wind turbine components cost reduction, and improving the control system reduces mechanical loads with minimum effort. In modern wind turbines, electricallyexcited synchronous generators are mostly applied in directdrive structure. In current research, generator field voltage along with the blade pitch angle is employed for tower load reduction in a novel multivariableadaptive control structure. The controller is designed based on the extracted model with aerodynamic, vibratory and electrical interactions. The centralized multivariable structure is chosen to simultaneously reduce rotor speed fluctuations and tower vibrations. Since the nonlinear wind turbine model is complex, the controller is designed via optimization process. The nonlinear aerodynamic behavior of blades influences the closedloop performance in different operating condition; therefore controller is adapted to the condition by employing gainscheduling method. The effects of signal noise, digital control and higherorder dynamics of electrical system might defect the closedloop stability. The designed controller is implemented on a wind turbine simulator which includes the previouslymentioned effects. By comparing the performance of the multivariable adaptive controller with a two inputone output multivariable controller, it is proven that the mechanical loads acting on tower have been greatly decreased...[]. Pleasecitethisarticleusing: : A. Hatami, B. MoetakefImani, A novel control structure for wind turbine with synchronous generator for tower load reduction, Modares Mechanical Engineering, Vol. 6, No., pp. 4553, 26 (in Persian)
2 ProportionalIntegralDifferentiator (PID) 6 Hardware In the Loop (HIL). [3].. [3,2]..[5,4]. [6]. [7]. [8]. 2.. [8,7] [9]... 3 ).. 4 Linear Quadratic Gaussian (LQG) 2 Linear Quadratic Regulator (LQR) 3 Electrically Excited Synchronous Generator (EESG) 4 foreaft
3 C q = =5 = =5 =2 = Fig. 2 Torque coefficient versus tip speed ratio for various pitch angle 2 C T Fig. 3 Thrust coefficient versus tip speed ratio for various pitch angle 3 Table Natural frequencies of tower in Hz ) = =5 = =5 =2 =25 Fig. 4 Four mode shapes of tower with concentrated tip mass 4 Fig. Interaction of aerodynamic, mechanical and electrical subsystems of wind turbine 2 [] (2) (). (3) = (, ) 2 = (, ) (2) 2 (3) = 3 2. () (4) + = = +, = +. (5)... [2,] 4 (4) (5)
4 Fig. 5 Block diagram of wind turbine nonlinear model with flexible tower 5 :[9,8] [2] ) ( ). ( ) (2).. 2 decentralize 3 centralize.[3] [4] = (6) [6,5] + = (6) (7) (7) 32 [7]. (8). () (9)..56 = [ ] (8).29 = (9) ( +.7).25( +.73) = () sideside
5 max( ) min( ) <.2, =,2,, 3) (2) (4). = / (4) (6) (5)..[8] = + + = + + (5) (6). 9. (7) PID gains (deg) Fig. 7 Pitch control gains as functions of pitch angle 7 3 gainscheduling k p k i k d Fig. 6 Closedloop nonlinear block diagram for wind turbine 6.. [22,2] () () = + + () (3) (2) 2 [23] 2 = ( ) < max( ) < 7, =,2,,.3 < min( ), =,2,,. < max( ) <.5, =,2,,. (2) 3) 3) 3) 2norm 2 norm
6 .[24] [2725] Fig. 9 Concentrated multivariable control structure 9 imaginary axis (rad/s) real axis (rad/s) Fig. Closedloop poles in splane Dapming ratio (%) V w to r V w to dx tip /dt V (m/s) w Fig. The variation of closedloop poles damping ratio with respect to wind speed (deg) V w (m/s) Fig. 8 Pitch angle variation above the rated wind speed for stable operation 8. (8) = + = [ ], = [ ], = (7) (8) (9).. (2) (2) = = + = = = + (22) 9) 9) 9) 9) 9) + + = 9) = (2) = + ( + ) + (2) = 22) = ( ) 22) = ( + ) 22) (23). () (). = = ( ) (24) (23) (24)... splane
7 [2] r (rpm) [28] % Fig. 3 Rotor speed via and controllers 3 dx tip /dt (mm/s) Fig. 4 Tower top velocity via and controllers 4. (). (4) (3 ) (2 ) 2 (6 ) (5) Table 2 Test setup components properties (deg) Fig. 5 Pitch angle via and controllers 5 2 Duty cycle Fig. 2 Test setup structure 2 MultiInput SingleOutput ()
8 (kgm 2 s ) (kgm 2 s ) (kgm 2 s ) (kgs ) (Ndeg ) (kgms 2 ) (Nsm ) (Nsrad ) (Av ) (rads N m ) (ms N ) (As) (m) (kgm 2 ) (kgm 2 ) (kgm 2 ) (kgs 2 ) (kgm 2 s 2 A ) (kg) (m) (m) (kgm 2 s 2 ) (kgm 2 s 2 ) (s) (v) (ms ) (m) (ms ) (ms 2 ) (deg) (deg) (kgm 3 ) (Nmdeg ) (Ns) (Nmsrad ) (rad/s) 8 V f (v) Fig. 6 Excitation voltage via and controllers x tip (mm) Fig. 7 Tower top displacement via and controllers 7 3 Table 3 Comparison of the multivariable controllers performance %
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