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1、 No. 6 CHE Wei-Wei and YANG Guang-Hong: Quantized Dynamic Output Feedback H Control for · · · 657 To facilitate the presentation of Theorem 2, we denote Aeopt = A Bcopt C2 B1 Ccopt , Ceopt = C1 Acopt 0 Acopt 0 Bcopt B1 0 D12 Ccopt By solving LMI (9, a controller is obtained with the g

2、ain matrices = Aini c 0.0213 0.9711 1.6320 3.1451 = , B ini c 5.0328 1.3363 0.2317 ¯1opt = B C ini = 0.0040 c Theorem 2. Consider plant (1 controlled by the quantized dynamic output feedback controller (6, if only M1 and M2 are chosen satisfying M1 > M2 > where opt = opt opt min (Qopt opt

3、 2 C2 min (Qopt (46 (47 2 2 = 1 + ( 3 + Ccopt 1 , opt T ¯ + opt min (Qopt with opt = Ceopt D1 + opt + T T ¯ T ¯ ¯1 ¯1 ¯ Aeopt Popt B1opt and opt = D D1 + 2B opt Popt B1opt . Then, the control strategy (6 with updating µ1 and µ3 by 2 opt µ1 = 2|x c | M1 +

4、opt opt min (Qopt , µ3 = µ1 (48 correspondingly, the value of is obtained as au = 3.6421. Let = 2 and the quantization errors 1 = 2 = 3 = 0.1. On the one hand, by Lemma 1 and Q( > 0 with the ini ini above gain matrices Aini c , B c , C c , and = 4.3346 and = 0.01, we obtain matrices Qle

5、m and Plem . Apparently, min (Qlem = 0.01. By Theorem 1, it is easy to compute /min (Qlem = 279.2494 and 2 C2 /min (Qlem = 663.0357. Let M1 = 280 > 279.2494 and M2 = 664 > 663.0357. According to (7, the range of the quantizer q3 (· can be computed as M3 = 7.5208. In contrast, by Algorithm

6、 1, with Ac0 = Aini c , B c0 = ini B ini c , C c0 = C c , = 0.0001, c0 = 1, c1 = 100, c2 = 10 000, and = 4.3346 and = 0.01, we obtain optimized matrices Qopt , Popt , and the controller gain matrices 0.0179 0.9454 1.4231 2.6540 , B copt = , 1.1833 4.6790 0.2317 . and updating µ2 by µ2 = 2|

7、y | M2 + opt 2 C2 min (Qopt Acopt = (49 C copt = 0.0040 renders the closed-loop system (8 asymptotically stable and with the H performance bound . Proof. It is similar to the proof of Theorem 1 and is omitted here. Remark 4. Because min (Q has a signicant eect on the value of /min (Q, the condition

8、Q( > 0 is introduced to restrict the value of min (Q, such that min (Q . Remark 5. On the one hand, in Algorithm 1, by means of optimizing the index , we obtain the optimized solutions Acopt , Bcopt , Ccopt , Popt , and Qopt , such that the values of opt opt /min (Qopt and opt 2 C2 /min (Qopt are

9、 minimum. Thus, the ranges M1 , M2 , and M3 can be optimized indirectly. On the other hand, by Theorem 2, when M1 > opt opt /min (Qopt and M2 > opt 2 C2 /min (Qopt , controller (6 with gain matrices Acopt , Bcopt , and Ccopt , by updating µ1 , µ3 according to (48 and updating µ2

10、 according to (49 renders the closed-loop system (8 asymptotically stable and with the H performance bound . So we have given an optimization method to solve Problem 1. By Theorem 2, we can obtain opt opt /min (Qopt = 244.3255 and opt 2 C2 /min (Qopt = 577.7594. Let M1 = 245 > 244.3255 and M2 = 5

11、78 > 577.7594. And according to (7, the range of the quantizer q3 (· can be computed as M3 = 6.5810. The quantizer ranges obtained by Theorem 1 and by Theorem 2 will be compared in Table 1. Table 1 Comparison of the quantizer ranges Theorem 1 Theorem 2 245 578 6.5810 M1 M2 M3 280 664 7.5208

12、3 Example In this section, an example is presented to illustrate the eectiveness of the proposed method. Example 1. Consider the system of form (1 with 0.5 1 B2 = 0 0.5 1 , B1 = , C1 = 1 .5 1 0 0.5 , C2 = 1 0 1 , D 12 = 0 1 1 0 A= From Table 1, it is clear that the ranges of the quantizers q1 (·

13、;, q2 (·, and q3 (· obtained by Theorem 2 are much more improved than the corresponding one obtained by Theorem 1, by reducing 12.58%, 12.19%, and 12.50%, respectively. The initial system state and controller state are chosen as x 0 = 5, 4 and x c0 = 10, 10, respectively. Let the disturban

14、ce input = 10 randn + 5 for k 15, 25, and let the disturbance input = 0 for all the other k, where randn is a normal distribution with mean zero, variance one, and standard deviation one. Then, Fig. 1 shows the regulated output responses of system (8. In Fig. 1, the solid lines show the results obta

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