Hu, Qinglei; Xiao, Bing Robust adaptive backstepping attitude stabilization and vibration reduction of flexible spacecraft subject to actuator saturation. (English) Zbl 1271.74156 J. Vib. Control 17, No. 11, 1657-1671 (2011). MSC: 74H45 93D21 PDFBibTeX XMLCite \textit{Q. Hu} and \textit{B. Xiao}, J. Vib. Control 17, No. 11, 1657--1671 (2011; Zbl 1271.74156) Full Text: DOI
Hu, Qinglei Neural network-based adaptive attitude tracking control for flexible spacecraft with unknown high-frequency gain. (English) Zbl 1193.93120 Int. J. Adapt. Control Signal Process. 24, No. 6, 477-489 (2010). MSC: 93C40 92B20 93D05 93C41 PDFBibTeX XMLCite \textit{Q. Hu}, Int. J. Adapt. Control Signal Process. 24, No. 6, 477--489 (2010; Zbl 1193.93120) Full Text: DOI
Hu, Qinglei A composite control scheme for attitude maneuvering and elastic mode stabilization of flexible spacecraft with measurable output feedback. (English) Zbl 1273.70056 Aerosp. Sci. Technol. 13, No. 2-3, 81-91 (2009). MSC: 70Q05 70M20 74H45 93B52 PDFBibTeX XMLCite \textit{Q. Hu}, Aerosp. Sci. Technol. 13, No. 2--3, 81--91 (2009; Zbl 1273.70056) Full Text: DOI Link
Hu, Qinglei Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits. (English) Zbl 1170.74338 Nonlinear Dyn. 55, No. 4, 301-321 (2009). MSC: 74H45 74M05 PDFBibTeX XMLCite \textit{Q. Hu}, Nonlinear Dyn. 55, No. 4, 301--321 (2009; Zbl 1170.74338) Full Text: DOI
Hu, Qinglei; Ma, Guangfu; Xie, Lihua Robust and adaptive variable structure output feedback control of uncertain systems with input nonlinearity. (English) Zbl 1283.93063 Automatica 44, No. 2, 552-559 (2008). MSC: 93B12 93B35 93B52 93C41 93C15 PDFBibTeX XMLCite \textit{Q. Hu} et al., Automatica 44, No. 2, 552--559 (2008; Zbl 1283.93063) Full Text: DOI
Hu, Qinglei Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics. (English) Zbl 1170.70388 Nonlinear Dyn. 52, No. 3, 227-248 (2008). MSC: 70Q05 70M20 74M05 74H45 PDFBibTeX XMLCite \textit{Q. Hu}, Nonlinear Dyn. 52, No. 3, 227--248 (2008; Zbl 1170.70388) Full Text: DOI
Hu, Qinglei; Ma, Guangfu Manoeuvring and vibration reduction of a flexible spacecraft integrating optimal sliding mode controller and distributed piezoelectric sensors/actuators. (English) Zbl 1266.93025 Int. J. Adapt. Control Signal Process. 21, No. 6, 452-476 (2007). MSC: 93B12 70P05 PDFBibTeX XMLCite \textit{Q. Hu} and \textit{G. Ma}, Int. J. Adapt. Control Signal Process. 21, No. 6, 452--476 (2007; Zbl 1266.93025) Full Text: DOI
Hu, Qinglei; Xie, Lihua; Gao, Huijun Adaptive variable structure and active vibration reduction for flexible spacecraft under input nonlinearity. (English) Zbl 1182.74091 J. Vib. Control 13, No. 11, 1573-1602 (2007). MSC: 74H45 93C40 PDFBibTeX XMLCite \textit{Q. Hu} et al., J. Vib. Control 13, No. 11, 1573--1602 (2007; Zbl 1182.74091) Full Text: DOI
Hu, Qinglei; Ma, Guangfu Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft. (English) Zbl 1293.93157 Eur. J. Control 12, No. 6, 654-668 (2006). MSC: 93B12 93B35 93B52 70P05 93C10 PDFBibTeX XMLCite \textit{Q. Hu} and \textit{G. Ma}, Eur. J. Control 12, No. 6, 654--668 (2006; Zbl 1293.93157) Full Text: DOI Link
Hu, Qinglei; Ma, Guangfu Control of three-axis stabilized flexible spacecraft using variable structure strategies subject to input nonlinearities. (English) Zbl 1182.70063 J. Vib. Control 12, No. 6, 659-681 (2006). MSC: 70Q05 93B52 74H45 PDFBibTeX XMLCite \textit{Q. Hu} and \textit{G. Ma}, J. Vib. Control 12, No. 6, 659--681 (2006; Zbl 1182.70063) Full Text: DOI
Hu, Qinglei; Ma, Guangfu Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver. (English) Zbl 1195.74120 Aerosp. Sci. Technol. 9, No. 4, 307-317 (2005). MSC: 74M05 74H45 74K10 PDFBibTeX XMLCite \textit{Q. Hu} and \textit{G. Ma}, Aerosp. Sci. Technol. 9, No. 4, 307--317 (2005; Zbl 1195.74120) Full Text: DOI