John Wen

Prof. John Wen

Rensselaer Polytechnic Institute
orcid

Research Focus & Metrics

Academic Career Length

39Years (1988-Present)

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

Representative Publications

View All Publications
1 January 1991 in IEEE Transactions on Automatic Control
Verified
Journal Article
Closed access
John WenJohn Wen
John Wen
KKK. Kreutz-Delgado
K. Kreutz-Delgado
A general framework for the analysis of the attitude tracking control problem for a rigid body is presented. A large family of globally stable control laws is obtained by using the globally nonsingular unit quaternion representation in a Lyapunov function candidate whose form is motivated by the consideration of the total energy of the rigid body. The controllers share the common structure of a proportional-derivative feedback plus some feedforward which can be zero (the model-independent case), the Coriolis torque compensation, or an adaptive compensation. These controller structures are compared in terms of the requirement on the a priori model information, guaranteed transient performance, and robustness. The global stability of the Luh-Walker-Paul robot end-effector controller is also analyzed in this framework.

1 December 1997 in Automatica
Verified
Journal Article
Closed access
RBRandal W. Beard
Randal W. Beard
GSGeorge N. Saridis
George N. Saridis
John WenJohn Wen
John Wen

1 March 1996 in IEEE Transactions on Automatic Control
Verified
Journal Article
Closed access
FLF. Lizarralde
F. Lizarralde
John WenJohn Wen
John Wen
It is well known that the linear feedback of the quaternion of the attitude error and the angular velocity globally stabilizes the attitude of a rigid body. In this note, we show that the angular velocity feedback can be replaced by a nonlinear filter of the quaternion, thus removing the need for direct angular velocity measurement. In contrast to other approaches, this design exploits the inherent passivity of the system; a model-based observer reconstructing the velocity is not needed. An application of the proposed scheme is illustrated for the robot control problem. Simulation results are included to illustrate the theoretical results.

1 October 1995 in IEEE Transactions on Automatic Control
Verified
Journal Article
Closed access
SJS.M. Joshi
S.M. Joshi
AKA.G. Kelkar
A.G. Kelkar
John WenJohn Wen
John Wen
This paper considers the problem of three-axis attitude stabilization of a rigid spacecraft. A nonlinear control law which uses the feedback of the unit quaternion and the measured angular velocities is proposed and is shown to provide global asymptotic stability. The control law does not require the knowledge of the system parameters and is, therefore, robust to modeling errors. The significance of the control law is that it can be used for large-angle maneuvers with guaranteed stability.<>

1 June 1997 in Smart Materials and Structures
Verified
Journal Article
Closed access
PDF file
DHDeclan Hughes
Declan Hughes
John WenJohn Wen
John Wen

19 February 2004 in IEEE Transactions on Automatic Control
Verified
Journal Article
Closed access
John WenJohn Wen
John Wen
MAM. Arcak
M. Arcak
Network flow control regulates the traffic between sources and links based on congestion, and plays a critical role in ensuring satisfactory performance. In recent studies, global stability has been shown for several flow control schemes. By using a passivity approach, this paper presents a unifying framework which encompasses these stability results as special cases. In addition, the new approach significantly expands the current classes of stable flow controllers by augmenting the source and link update laws with passive dynamic systems. This generality offers the possibility of optimizing the controllers, for example, to improve robustness in stability and performance with respect to time delays, unmodeled flows, and capacity variation.