> P R;w > > : 0
if
v < V ci
if V ci < v < V r if V r < v < V co if
ð19Þ
v > V co
A, B and C are coefficients which are extracted from [19]: The cost of generating wind power includes investment cost, operation and maintenance cost. It can be formulated as MT cost and computed as Eq. (20):
during the faults. This operation scenario of battery is similar to DGs except that the available power of battery during failure events depends on the amounts of its stored power in past. The battery should be discharged during the faults and supply the load buses according to their priority. The power which will be produced by battery in Eq. (5), computed in Eq. (27).
PRES ST;i ðt; l; r k Þ ¼
X
¼
dð1þdÞ I ð1þdÞ þ C o&m;wt n 1
P R;w CF wt 8760
Pwt t
¼
0;
ð21Þ
The battery SOC is modeled according to Eq. (22) [21].
Pbat ðtÞ Dt SOC ðt þ Dt Þ ¼ SOCðtÞ þ gbat V base
ð22Þ
2.2.5. PV cost modeling The outage power of PV depends on cells temperature and solar irradiance in Maximum Power Point (MPP) linearly that can be formulated as follows [22]:
GT ðtÞ PPV ðtÞ ¼ PPV ;STC 1 c T j T jSTC NPVs N PVp GT STC ð23Þ GT ðtÞ ðNOCT 20Þ GT STC
ð24Þ
According to Eq. (25), solar power generating cost includes investment, power electronic interfaces, operation and maintenance, and installation costs.
CF OPR PV;t ¼ C Inv ;PV þ C o&m þ C Ins;PV þ C SollarPanel;PV
ð25Þ
2.2.6. Reliability cost modeling In current work, the ENS value is considered as reliability index, and the MG operator is penalized according to this index. The penalty cost value depends on the not supplied energy levels. The proposed algorithm tries to decrees penalty cost like the other MG costs by optimal operation. Therefore, the islanding mode operation capability will be important. DGs and battery are used to restore lost loads in failure events periods. After each failure event the faulty parts will disconnect from the rest of MG by the circuit breakers located at two sides of feeders. The DGs located at the faulty parts should not only supply lost loads according to their priority, but also have the ability of supplying them (in this paper all load demands have the same priority). The restoration power of DGs, as mentioned in Eq. (5), can be computed as Eq. (26) after restoration of faulty part. [15]
X
yDG ði; LÞ P FCAP DG;i;L ;
yDG ði; LÞ
L2NDG
¼
Otherwise
2.3. Uncertainty modeling
CF OPR Battery;t ¼ C o&m;battery þ C Inv ;battery þ C Pow:Elec:;battery þ C wc;battery
PRES DG;i ðt; l; r k Þ ¼
ð27Þ
1; if ith load is connected to Lth Storage
ð20Þ
2.2.4. Battery cost modeling The operational cost of batteries includes wear cost, operation and maintenance cost, investment cost and the power electronic interfaces cost as Eq. (21). The wear cost will be computed based on [20].
T j ¼ T amb þ
yST ði; LÞ
L2NST
n
CF OPR Wt;t
yST ði; LÞ P FCAP ST;i;L ;
1; if ith load is connected to Lth DG 0; Otherwise
The uncertainty is defined as the probability of difference between the forecasted value and the real value. The exact modeling of renewable resources and load uncertainties has a significant effect on MG operational cost. There are different methods to deal with uncertainties such as analytical methods, and approximate methods and so on, which can be used in different problems optimally with regard to their application. 2.3.1. Wind and solar power uncertainties modeling based on PEM method PEM method fundamental PEM is one of the approximate methods, which deals with uncertainties. This method is favorite for power system operators because of its high accuracy in computing and its needless to have information of random variables PDF. Km + 1 Hong’s PEM Concentrating statistical information of a random variable on K points, which a function ðFÞ establishes a connection between input variables (probabilistic (XÞ and deterministic (cÞÞ and output variables, is the main idea of PEM. Function F (Z ¼ F ðp1 ; p2 ; . . . ; pl ; . . . ; pm ; cÞÞ depends on all input variables (mÞ. According to Fig. 2, in Hong’s PEM, for each random variable ðpl Þ, function F should be computed Km + 1 times where K is the number of points and l = 1, 2, 3, . . ., m. The K points related to the m random variables ðpl;k ; xl;k Þ will be computed based on statistical information and the PDF of that variable. This computed pair data for each random variable includes pl;k and its weighting factor xl;k , which states the weight of the location in output results. The location pl;k is computed as follow:
pl;k ¼ lpl þ nl;k rpl
ð28Þ
z Z=f(P1,P2,…,Pl,…,Pm)
(z(l,2), l2)
(z(l,3), 0)
(z(l,1), l1)
fpl ð26Þ
In this paper, the storage system is used to supply not only load demands at peak time, but also required energies of load demands
pl
Fig. 2. 2m + 1 Scheme.
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where lpl , rpl , nl;k denote the mean, the standard deviation of input
Start
random variable pl and the standard location of kth point respectively. The standard location nl;k and weighting factors xl;k will be computed by solving the nonlinear equations set which are stated in Eq. (29) [23].
8 K X > > > xl;k ¼ m1 > < k¼1
Input micro-grid data, selling and purchasing energy costs, DGs operation and pollution costs, battery operation cost, the mean value and variance of wind speed and solar irradiance at the next day
Uncertainty modeling of wind power and solar power using 2 m +1 PEM and extracting [(w 1,w 2,w 3),(Pw 1,Pw 2,Pw 3)], [(w 1,w2,w3),(Pv 1,Pv 2,Pv 3)] using Eqs. (28-31) and (33, 34)
ð29Þ
K > X > > > xl;k nl;k j ¼ kl;j :
j ¼ 1; . . . ; 2K 1
k¼1
Define
and determine the uncertain hours of load demand randomly
where kl;j is the jth standard central moment of random variable pl with density function f pl . The standard central moments can be computed as follow:
h =1
Extract the h th sample of load demand profile using Eqs. (42-46)
Mj ðp Þ kl;j ¼ l j
ð30Þ
rpl
Initialize particles of PSO
where M j ðpl Þ, is calculated by Eq. (31).
M j ðpl Þ ¼
Z
1
1
j pl lpl f pl dpl
k=1
ð31Þ
Start the k th iteration of PSO
It should be noticed that kl;1 ¼ 0; kl;2 ¼ 1, and kl;3 ; kl;4 are the skewness and kurtosis of pl , respectively. How to solve Eq. (29) is completely described at [24]. After computing all pairs ðpl;k ; xl;k Þ, the output function Z will be computed for each variable and for each concentrated point Zðl; kÞ based on Fðlp1 ; lp2 ; . . . ; pl;k ; . . . ; lpm Þ. The output random variable in
Calculate the objective function for the operation period using Eq. (1)
Calculate the expected values of power flow results (DGs, battery and Grid optimal operating points) using Eq. (32)
jth moment will be computed according to Eq. (32).
EðZ j Þ ffi
m X K X
h
xl;k F lp1 ; lp2 ; . . . ; pl;k ; . . . ; lpm
i j
Update the global and previous particle and velocity
ð32Þ
l¼1 k¼1
Move the particles
In current work, (2m + 1) Hong’s PEM scheme (K ¼ 3; nl;k ¼ 0Þ is applied for wind and PV power uncertainties. K ¼ 3 is selected for each input random variable, and the third point is placed in mean value of the variable. Then, the first forth moments of the random variable PDF should be computed. The essential equations to compute nl;k and xl;k are taken from [25] as follow:
rffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi kl;3 3 3k kl;4 k2l;3 k ¼ 1; 2 nl;3 ¼ 0 nl;k ¼ þ ð1Þ 4 2 ð1Þ3k 1 1 xl;k ¼ ; xl;3 ¼ m kl;4 k2l;3 nl;k ðnl;1 nl;2 Þ
Is PSO algorithm converged ?
ð33Þ
Is PSO algorithm converged ?
ð34Þ
x0 ¼
xl;3 ¼ 1
l¼1
1
l¼1
kl;4 k2l;3
Yes
Modify the robust optimal solution
No
h=h+1
No
Is PSO algorithm converged ? Yes
function F in this point and its new weighting factor should be computed (x0 Þ. m X
k=k+1
Yes
According to Eq. (28), setting nl;3 ¼ 0, yields pl;k ¼ lpl , therefore the third point of all random variables will be their mean values lp1 ; lp2 ; . . . ; lpl ; . . . ; lpm . So there is one more computation of
m X
No
Save the most robust results
ð35Þ
WT and PV uncertainties modeling In this paper, wind speed and solar irradiance are considered as two random variables and function F is power flow equations which their results are the voltages of busses and the exchanging power with upstream distributed network in slack bus (the slack bus is the 20/0.4 kV substation bus). Weibull PDF and Beta PDF are applied to deal with uncertainties related to the wind speed and solar irradiance, respectively. Solar irradiance modeling According to [26], Beta PDF is the best distribution function to model solar irradiance that is formulated as follow:
Finish
Fig. 3. The proposed algorithm flow chart.
( f b ðxÞ ¼
CðaþbÞ CðaÞCðbÞ
0
xa1 ð1 xÞb1
for 0 6 x 6 1; a P 0; b P 0 Otherwise ð36Þ
In Eq. (36), x is the amount of solar irradiance in kW/m2, a and b are Beta PDF parameters and f b ðxÞ is the Beta PDF of x. a and b will be
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Power Utility Grid
20 Kv 400 V SD
400 V
PCC
Bus. 1
Bus. 11
Feeder 3. Commercial
Bus. 8
Bus. 3
Feeder 2. Residential
Feeder 1. Residential
Bus. 7
Bus. 2
Bus. 6 Bus. 12 Disel Generator
Bus. 9
Bus. 4
Bus. 13 Bus. 5
Bus. 10 Bus. 14
Micro Turbine
PV
Battery Bank Wind Turbine Fig. 4. The proposed MG topology.
computed by use of mean value ðlÞ and standard deviation (rÞ of random variable x according to Eqs. (37) and (38):
lð1 þ lÞ 1 r2
lð1 þ lÞ 1 b ¼ ð1 lÞ r2
a¼l
ð37Þ ð38Þ
Wind speed modeling According to the [26], Weibull PDF is the best distribution function to model wind speed behavior, which is formulated in Eq. (39).
k1 h V wind k i k V wind c f w ðV wind Þ ¼ e c c
ð39Þ
where k is called the shape index, and c is called the scale index.
2.3.2. Load uncertainties modeling based on RO RO fundamental RO, first was introduced by Soyster in 1973, uses uncertain boundaries to describe the input variables uncertainties. Applying this method leads to the proper decisions which will be optimized for the worst case of probabilistic input variable into the determined boundary. The main application of this method is when there is not enough data for the input variable PDF. If function Z ¼ f ðxÞ depends on uncertain input x, because of the lack of a certain PDF of x, its uncertainty will be modeled as an uncertain boundary x 2 UðxÞ which according to Eq. (40), x can choose every value in boundary U.
x 2 UðxÞ ¼ fxjjx xj 6 ^xg
ð40Þ
In Eq. (40), x and ^x are the forecasted value and the possible maximum difference between x and x. RO seeks a way not only to
S.A. Alavi et al. / Energy Conversion and Management 95 (2015) 314–325
Residential Load (%),Commercial Load (%), Price of Purchasing Energy (%) Price of Selling Energy (%)
320
100 Price of Purchasing Energy Price of Selling Energy Commercial Load Residental Load
90 80 70 60 50 40 30 20 2
4
6
8
10
12
14
16
18
20
22
24
Time (h) Fig. 5. Load and price profiles.
45
Wind power Solar power
40 35
(kW)
30 25 20 15 10 5 0
1
2
3
4
5
6
7
8
9
10 11 12 13 14 15 16 17 18 19 20 21 22 23 24
Time (h) Fig. 6. Mean value of wind power and solar power.
Table 1 Result of running program in Sc.2, Sc.3, Sc.4 with C ¼ 5. Time (h)
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24
Scenario 2
Scenario 3
Scenario 4
Diesel Generator
Micro Turbine
Battery
Grid
Diesel Generator
Micro Turbine
Battery
Grid
Diesel Generator
Micro Turbine
Battery
Grid
0 0 0 0 0 0 95.53 92.1 0 0 92.26 0 0 81.41 87.09 75.09 0 321.38 400 400 352.12 327.49 98 0
300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300
39.27 0 39.27 39.27 33.14 0 39.27 0 0 0 0 0 0 0 0 0 0 39.27 39.27 39.27 38.99 0 0 0
133.14 72.77 112.94 115.11 107.26 106.44 83.45 106.76 263.61 261.07 176.06 266.89 174.08 179.93 172.22 176.13 263 0 30.95 9.9 0 0 188.62 164.04
0 0 0 0 0 0 94.86 85.46 0 84.94 0 86.26 87.05 0 0 0 0 310.87 400 383.1 382.72 400 0 0
300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300
0 0 0 39.27 20.31 0 39.27 39.27 0 0 0 0 0 0 0 0 0 39.27 39.27 39.18 0 0 0 0
89.1 64.45 62.63 110.58 86.55 103.1 78.97 150.66 258.21 163.1 263 172.55 179 246.87 243.27 237.56 250.15 0 16.28 0 0 89.14 278.59 155.95
0 0 0 0 0 0 99.6 0 0 0 91.38 81.17 81.94 0 0 76.44 0 351.3 400 400 335.69 306.72 0 0
300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300 300
0 39.27 0 0 0 39.27 39.27 0 0 0 0 39.27 0 0 0 0 0 0 39.27 0 39.27 0 39.27 14.14
89.05 122.95 48.02 70.34 65.82 143.39 74.21 177.12 258.21 248.56 171 217.56 184.1 246.87 243.27 160.68 250.15 0 16.28 22.93 0 0 214.6 141.51
Voltage (p.u)
Voltage (p.u)
Fig. 7. Buses voltage profiles in Sc.1 (a), Sc.2 (b), Sc.3 (c), and Sc.4 (d).
1.01 1
1.02
1.03
1.04
1.05
1.06
1.01 1
1.02
1.03
1.04
1.05
5
5
10
10
Time (h)
15
Time (h)
15
20
20
(b)
24
(a)
24
14
14
13
13
12
12
11
11
10
10
8
6
7
Bus Number
8
6
Bus Number
9
9
7
5
5
4
4
3
3
2
2
1
1
Voltage (p.u) Voltage (p.u)
1.06
1.01 1
1.02
1.03
1.04
1.05
1.06
1.01 1
1.02
1.03
1.04
1.05
1.06
5
5
Time (h)
15
15
Time (h)
10
10 20
20
(d)
24
(c)
24
9
7
6
Bus Number
8
6 8 7 10 9 11 12 14 13 Bus Number
14 13
10 12 11
5
5
4
4
3
3
2
2
1
1
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optimize the cost function but also to reach optimized solution with high probability, when there is error in forecasted value of variable x [27–31]. Load uncertainty modeling In this paper, the load demands of busses ðPload Þ that can fluctuate into a boundary are considered as random variables, also we consider load demand with not adequate information of its PDF but bounded. Therefore, with regard to [1,30] RO will be a proper method to model load demand uncertainty. The RO modeling procedure can be explained as follow: For each load demand in each interval a boundary like as Eq. n (41) and a forecasted value plbt , is associated.
^lcbt ; p ^ltbt plbt 2 ½p
ð41Þ
^ltbt and p ^lcbt are upper and lower bound of load demand In Eq. (41), p for every load bus in any b and t. In RO, the cost function will be optimized for the worst case of possible event while reaching this worst case is a complicated problem. In this method, a Conservation Degree (CD) (C) is defined (C is the number of time periods that plbt n is allowed to be different from its forecasted value plbt ) that in this paper, C 2 ½0; T. If C = 0; therefore, the real value of load demand is close to the forecasted value in every period of operating and if C = t, so in t arbitrary hours in the operating time period the value of real load demand is different from the forecasted value [27,28]. With increasing C, the optimization process will be more robust while the optimization cost increases. Thus, selecting the suitable C for each optimization problem in each work condition is different. In order to determine the uncertain set, first, axillary variables should be defined like Eqs. (42)–(44) and then the uncertain set will be defined. 2500
2344.8
Cost ($)
2000 1500
1445.9
1448.9
1457.8
Sc.2
Sc.3
Sc.4 , =5
1000 500 0
Sc.1
Fig. 8. MG operational cost in Sc.1, Sc.2, Sc.3, Sc.4 with C = 5.
8 þ if plbt ¼ p^ltbt > < zbt ¼ 1 ^lcbt z ¼1 if plbt ¼ p > : bt n þ zbt ¼ zbt ¼ 0 if plbt ¼ plbt c n c ^lbt plbt ¼ plbt p
ð42Þ ð43Þ
t
^ltbt plnbt plbt ¼ p
ð44Þ
Using Eq. (42)–(44), the uncertain set will be defined as (45). ( ) T X þ n t c U ¼ pl 2 RjBjT : zbt þ zbt 6 Cb ;pl ¼ plbt þ zþbt plbt zbt plbt 8b 2 B; 8t 2 T t¼1
ð45Þ
Then, using Monte Carlo sampling method, different scenarios of load demand in each hour will be generated by a random variable (rv) subject to uniform distribution over [0 1] like Eq. (46):
8 n c þ if r v 6 Cb =2T > < pl ¼ plbt plbt ; zbt ¼ 0; zbt ¼ 1; n t zþbt ¼ 1; zbt ¼ 0; if r v P 1:2 Cb =2T pl ¼ plbt þ plbt ; > : n zþbt ¼ zbt ¼ 0; Otherwise pl ¼ plbt ; ð46Þ Therefore, the problem will be solved with different scenarios for deterministic pls and the possible worst event case will be optimized and will be recommended as the most robust solution. 3. Proposed methodology based on PSO algorithm Optimal energy management in a MG is a combinatorial problem which should be solved using powerful meta-heuristic methods. Due to the suitable capabilities in dealing with such problems, the PSO algorithm has been employed to solve the problem [32,33]. PSO is a swarm intelligent algorithm and it is based on the movement of some groups of particles, which share their explorations among themselves. Each individual in PSO called particle flies in the searching space with a velocity, which is dynamically adjusted according to its own flying experience and its components’ flying experience. The details of PSO can be found in [34,35]. The optimal energy management procedure is shown in Fig. 3. Using PDFs for modeling the uncertainties related to the wind power and solar power, the PEM determines three estimated points for wind power using Weibull distribution and three estimated points for solar power using Beta distribution with their weighting factors. This data will be saved into a matrix, then using RO method, different scenarios according to the CD (C), are made for the next day. The PSO algorithm is applied to determine the
Battery State Of Charge (SOC %)
80 Sc.2 Sc.3 Sc.4, gama=5
70 60 50 40 30 20 10 0
0
1
2
3
4
5
6
7
8
9
10 11 12 13 14 15 16 17 18 19 20 21 22 23 24
Time (h) Fig. 9. The battery SOC.
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optimal amount of output power of each DG, the battery scheduling as well as the amount of exchanging energy with upstream network in each interval of operating period based on minimizing objective function. According to the proposed flowchart (Fig. 3), the PSO algorithm with regard to decision variables, finds the best answers. The first results of PSO will be saved and RO, which seeks the most robust solution, generates and transfers the other load demand scenarios to the PSO algorithm. 4. Simulation results The proposed algorithm is used in order to perform an optimal operation of a Low Voltage (LV) MG including renewables and conventional DGs as well as a battery bank. The MG includes two residential feeders and one commercial feeder as shown in Fig. 4. The MG data is extracted from Ref. [36]. In order to facilitate operating in islanding mode, two circuit breakers are improvised in both ends of feeders; they disconnect the faulty parts of MG from the rest of the MG. In addition, this MG is capable to switch into islanding mode with regard to the technical or economic aspects by help of a Static switch (SD) which is installed in Point of Common Coupling (PCC) [19]. According to Fig. 4, DGs are located just in residential busses. In order to assess the accuracy of the proposed optimal operation procedure, it is done for different scenarios and their result will be compared with each other. It is required to mention that in all scenarios the exact values of [SOC min ,SOC max ] and [V bus;min ,V bus;max ] are [4, 80]% and [0.95, 1.05] p.u. respectively. The forecasted load demand in 24 h of operation period and the energy price are shown in Fig. 5, which 1490
1470 1460 1450 1440
1448.9
1430
Γ =0
1471.4
1474.3
Γ =10
Γ =15
1483
1486.2
Γ =20
Γ =24
1457.8 Γ =5
Fig. 10. MG operational cost in Sc.4 for different CDs.
Scenario 1: None of DGs (Sc.1) In this scenario, we assume that none of DGs and batteries are installed, so MG should purchase all of its required energy from the upstream distribution network. In this scenario, the MG operating cost includes the cost of purchasing energy with regard to the prices, which are presented in Fig. 5, and the cost of ENS calculated by Eq. (5). MG reliability is low in this scenario and with occurring any failure event in feeders, the related part will be disconnected and it will become without supplier. Scenario 2: Deterministic Energy management (Base case (Sc.2)) In this scenario, all DGs and the battery are added to the MG, and all random variables (wind speed, solar irradiance and load demand) are considered as deterministic. Therefore, a deterministic optimization problem is created with regard to the aforementioned cost function and constraints. In Sc.2, load demand is the same as Fig. 5, and the mean value of wind power and solar power are illustrated in Fig. 6. In Fig. 6, the mean values of wind power and solar power are computed by Eqs. (19) and (23), also the availability of mean values of wind speed and solar irradiance for each hour respectively. Fig. 6 describes that the maximum of PV output occurs at 14:00 and the maximum of WT output occurs at 17:00. Scenario 3: Half probabilistic operation (Sc.3) In this scenario the output power of WT and PV are modeled probabilistically and load demand is modeled deterministically. PEM determines three estimated points for both wind speed and solar irradiance and the optimization problem will be solved subject to these points and their weighting factors. Scenario 4: full probabilistic operation (Sc.4) This scenario uses all parts of the proposed algorithm with regard to the Fig. 3, and finds the most robust and optimal solution. PEM method is applied to deal with the WT and PV uncertainties and RO optimization method is applied to deal with load demand uncertainty. This problem has been solved for different CDs in order to show the sensitivity of operation procedure and MG total cost over the CD (C).
2100 Sc.4 CD=15 Sc.2 Sc.4 CD=24 Sc.4 CD=5 Sc.4 CD=10 Sc.4 CD=20 Sc.3
2050 2000 1950 1900
operation cost ($)
Cost ($)
1480
are normalized and stated in percent. In Fig. 5, the maximum power of residential and commercial load demand for each bus are 60 kW and the maximum energy purchasing and selling price are 24 and 16 Cent/kW respectively. The MG elements characteristic presented in Appendix.
1850 1800 1750 1700 1650 1600 1550 1500 1450 1400
0
2
4
6
8
10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40 42 44 46 48 50 52 54 56 58 60
Iteration Fig. 11. Convergence characteristics of scenarios in the case of cost objective.
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The numerical results of MG optimal optimization in Sc.2 to Sc.4 are shown in Table 1. According to the Table 1, the diesel generator due to producing pollution is only used in peak time of load demand which the price of purchasing energy from the upstream distribution network is high, and in low price hours this DG is not used or is used less than 25 % of its rated power. In addition, the MT optimal output power should be always in its rated power due to the load level and the cost of start-up considered for it. Moreover, the battery optimal charge and discharge power follow the authorized boundary and the rest of related constraints. Battery starts to charge in low energy price and off-peak hours and then starts to discharge in high energy price and on-peak hours in order to decrease MG costs. The optimal schedule of purchasing energy from the upstream distribution network is stated as follows: when the price of electricity is high, MG does not purchase energy or purchases a little energy or even it can sell energy to the distribution network. Applying the proposed optimal operation scheduling, the bus voltages will become as Fig. 7. According to the Fig. 7, it can be realized that the authorized bus voltage boundary is observed in all scenarios. This constraint is a considerable issue that should be observed in operation of distribution systems. Moreover, Fig. 7 demonstrates that when there is not any installed DG in MG (Fig. 7.a) the bus voltage drops in direct relation to its distance from the slack bus. Adding DG units to the busses of the MG (Fig. 7.b to d) results in increasing the bus voltage, when the installed DG is generating power, in comparison to that not having any DG unit. The total operational cost of MG in Sc.1–Sc.4 is depicted in Fig. 8. It is noticeable that applying DGs as well as battery unit in a MG system will decrease total operational cost, as in by comparing total cost in Sc.1 and Sc.3 we can find out that the total cost in Sc.3 decreased about 896 dollars whereas the MG reliability increased. The Optimal Charge and discharge of the battery has an important effect on decreasing MG total cost. Fig. 9 shows the SOC of battery in operation during in Sc.2, Sc.3 and Sc.4. In (Sc.4), the deviations of DPtLoad is bounded into a specified boundary [4% +5%]. Selecting C equals to zero means that the load demand profile of 24 h of the day is completely deterministic which was analyzed in (Sc.3) and the MG total operational cost was 1448.9 dollars. The optimal operation is applied on MG for different CDs 5, 10, 15, 20, 24 which the results for C ¼ 5 are shown in Table 1, and for the other CDs just the total operational cost has been extracted in this paper. The sensitivity of MG operational cost over CD is depicted in Fig. 10. According to Fig. 10, it is obvious that increasing CD results in rising MG operational cost while the operation will be more robust against load demand uncertainty. Fig. 11 also indicates the convergence characteristics of all scenarios in the case of cost objective.
5. Conclusion In this paper, an optimal strategy for operating a MG with the capability of operating in islanding mode is proposed. The uncertainty related to WT output power; PV output power and load demand were modeled successfully by PEM method and RO respectively, and decreased the operation risk. The numerical results showed that applying the proposed procedure decreased the MG operation cost significantly. Moreover, by increasing C, the system conservation and the operation cost increased while its risk decreased. In addition, both the islanding capability of MG and the presence of DGs decreased the amount of MG energy not supplied and increased the reliability of system.
Appendix Table Ap. 1 Installed DG source. ID
Type
Min
Max
1 2 3 4 5
Micro-turbine Diesel generator Battery PV WT
0 0 235.6 (kW h) 0 0
300 (kW) 400 (kW) +235.6 (kW h) 92 (kW) 250 (kW)
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