ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (9): 327434-327434.doi: 10.7527/S1000-6893.2022.27434
• Electronics and Electrical Engineering and Control • Previous Articles Next Articles
Jiajie CHEN1, Jiqiang WANG2(), Haibo ZHANG1, Zhongzhi HU3, Xinmin CHEN2
Received:
2022-05-13
Revised:
2022-07-05
Accepted:
2022-08-03
Online:
2022-09-01
Published:
2022-08-31
Contact:
Jiqiang WANG
E-mail:wangjiqiang@nimte.ac.cn
Supported by:
CLC Number:
Jiajie CHEN, Jiqiang WANG, Haibo ZHANG, Zhongzhi HU, Xinmin CHEN. Design of steady-state disturbance rejection controller for aeroengine based on geometric design method in finite frequency range[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 327434-327434.
Table 2
Realistic performances and transfer functions designed by GDM under different single frequency
GDM单频控制器传递函数 | ||||
---|---|---|---|---|
3 | (-1.13, -0.04) | 0.135(-17.4 dB) | 0.237(-12.5 dB) | |
8 | (-1.13, -0.04) | 0.143(-16.9 dB) | 0.378(-8.4 dB) | |
15 | (-1.13, -0.03) | 0.137(-17.3 dB) | 0.5(-6 dB) |
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