2014
DOI: 10.1177/1687814020927832
|View full text |Cite
|
Sign up to set email alerts
|

Adaptive H-infinity tracking control for microgyroscope

Abstract: An adaptive H-infinity tracking control is proposed for a z-axis microgyroscope with system nonlinearities. All the signals can be guaranteed in a bounded range, and tracking error is uniformly ultimately bounded, an H-infinity tracking performance is also achieved to a prescribed level. Adaptive control methodology is integrated with H-infinity control technique to achieve robust adaptive control, and adaptive algorithm is used to estimate the unknown system parameters. Simulation studies for microgyroscope a… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
4
0

Year Published

2020
2020
2023
2023

Publication Types

Select...
5

Relationship

0
5

Authors

Journals

citations
Cited by 5 publications
(4 citation statements)
references
References 31 publications
0
4
0
Order By: Relevance
“…Furthermore, the unknown system parameters are estimated by using an adaptive law. The difference between our studies and [18,19,21], and [20] is that we apply the nonsingular fast terminal sliding mode control with an adaptive law technique to achieve finite-time synchronization between two different chaotic systems with unknown parameters and disturbances.…”
Section: Design Of Finite-time Sliding Mode Controllermentioning
confidence: 97%
“…Furthermore, the unknown system parameters are estimated by using an adaptive law. The difference between our studies and [18,19,21], and [20] is that we apply the nonsingular fast terminal sliding mode control with an adaptive law technique to achieve finite-time synchronization between two different chaotic systems with unknown parameters and disturbances.…”
Section: Design Of Finite-time Sliding Mode Controllermentioning
confidence: 97%
“…Step 2. Consider control law (11). it's difficult to derive ν, ẑ1 , ẑ2 , and σO values analytically.…”
Section: Nonlinear H ∞ Attitude Controller and Modal Observermentioning
confidence: 99%
“…A flexible spacecraft body consists of a rigid hub and flexible appendages. In the literature, the spacecraft hub attitude angles are often selected as the attitude dynamic model's output [4,[6][7][8][9][10][11][12][13][14][15][16][17][18][19][20][21][22][23]. In this approach, the flexible appendages' vibration effect is considered as an unknown vibrational disturbance torque and the attitude controller should overcome, in addition to the model uncertainties and the environmental disturbances.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation