Qing Zhao

Prof. Qing Zhao

orcid

Research Focus & Metrics

Academic Career Length

29Years (1998-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 October 1998 in Automatica
Verified
Journal Article
Closed access
QZQing Zhao
Qing Zhao
JJJ. Jiang
J. Jiang

10 July 2006 in IEEE Transactions on Automatic Control
Verified
Journal Article
Closed access
APA.M. Pertew
A.M. Pertew
HMH.J. Marquez
H.J. Marquez
QZQing Zhao
Qing Zhao
The problem of observer design for Lipschitz nonlinear systems is considered. A new dynamic framework which is a generalization of previously used Lipschitz observers is introduced and the generalized sufficient condition that ensures asymptotic convergence of the state estimates is presented. The equivalence between this condition and an H/sub /spl infin// optimal control problem which satisfies the standard regularity assumptions in H/sub /spl infin// optimization theory is shown and a parameterization of all possible observers is also presented. A design procedure which is less restrictive than the existing design approaches is proposed, and a simulation example is given to illustrate the observer design.

1 August 2007 in Automatica
Verified
Journal Article
Closed access
APA.M. Pertew
A.M. Pertew
HMH.J. Marquez
H.J. Marquez
QZQing Zhao
Qing Zhao

14 March 2013 in Journal of the Franklin Institute
Verified
Journal Article
Closed access
CGChunyan Gao
Chunyan Gao
QZQing Zhao
Qing Zhao
GDGuangren Duan
Guangren Duan

3 May 2021 in IEEE Transactions on Industrial Electronics
Verified
Journal Article
Closed access
ZLZong-Yang Lv
Zong-Yang Lv
YWYuhu Wu
Yuhu Wu
QZQing Zhao
Qing Zhao
XSXiming Sun
Ximing Sun
In this article, the design and control of a new coaxial tilt-rotor unmanned aerial vehicle (CTRUAV) are presented. The CTRUAV is an electric-powered unmanned aerial vehicle with a special configuration, which is composed of two pairs of tiltable coaxial rotors and a rear rotor. A CTRUAV prototype has been designed by 3-D computer-aided design software and constructed according to the designing scheme. The dynamic model of a CTRUAV is derived by utilizing the Euler–Lagrange equation, which considers the special features of the coaxial rotors and air drag forces on the CTRUAV. An adaptive controller is developed to realize motion control for the CTRUAV. The adaptive controller includes two subcontrollers: an inner-loop attitude controller and an outer-loop velocity controller. The stability of the resulting closed-loop CTRUAV system is analyzed via the Lyapunov method. Finally, several simulations and real experimental tests are implemented to validate the effectiveness of the developed CTRUAV system.

31 January 2022 in Control Engineering Practice
Verified
Journal Article
Closed access
ZLZongyang Lv
Zongyang Lv
QZQing Zhao
Qing Zhao
SLShengming Li
Shengming Li
YWYuhu Wu
Yuhu Wu