Add to ORKGA direct adaptive actuator failure compensation scheme for satellite attitude control systems Yajie Ma1, Bin Jiang1, Gang Tao1,3 and Yuehua Cheng2 A new direct adaptive failure compensation approach is developed for satellite attitude control systems in the presence of uncertain failures of redundant actuators. The adaptive failure compensation controller is designed via a backstepping design, which can accommodate uncertainties in actuator failure time instants, values, and patterns. The failure uncer-tainties are estimated directly by adaptive laws and the adaptive satellite attitude control system with actuator failures is analyzed, to show its desired stability and asymptotic tracking properties. Finally, simulation results of a satelli...
This article investigates the attitude stabilization problem of a rigid spacecraft with actuator sat...
In a control system, actuator failures may cause significant damaging effect on system performance o...
This paper studied the trajectory tracking control of a failure satellite that has actuator jumping ...
A direct adaptive actuator failure compensation scheme for satellite attitude control systems Yajie ...
Spacecraft play an increasingly important role in various areas of modern society, such as telecommu...
Published version of an article in the journal: Mathematical Problems in Engineering. Also available...
Future spacecraft are expected to achieve highly accurate pointing, fast slewing from large initial ...
Today, more satellites are being launched at a rate never experienced before. This is due, in part, ...
This paper proposes a novel adaptive fault tolerant control strategy for flight systems which have n...
This paper proposes a novel adaptive fault tolerant control strategy for flight systems which have n...
Thousands of satellites are now in operation for various purposes such as communication, navigation,...
An actuator fault-tolerant attitude control was reported. Two kinds of spacecraft actuator failures ...
This paper designs an active fault-tolerant control system for spacecraft attitude control in the pr...
In this paper, an improved robust model predictive controller (RMPC) is proposed based on model refe...
Actuator failures onboard spacecraft often lead to unsatisfied control performances or even the lose...
This article investigates the attitude stabilization problem of a rigid spacecraft with actuator sat...
In a control system, actuator failures may cause significant damaging effect on system performance o...
This paper studied the trajectory tracking control of a failure satellite that has actuator jumping ...
A direct adaptive actuator failure compensation scheme for satellite attitude control systems Yajie ...
Spacecraft play an increasingly important role in various areas of modern society, such as telecommu...
Published version of an article in the journal: Mathematical Problems in Engineering. Also available...
Future spacecraft are expected to achieve highly accurate pointing, fast slewing from large initial ...
Today, more satellites are being launched at a rate never experienced before. This is due, in part, ...
This paper proposes a novel adaptive fault tolerant control strategy for flight systems which have n...
This paper proposes a novel adaptive fault tolerant control strategy for flight systems which have n...
Thousands of satellites are now in operation for various purposes such as communication, navigation,...
An actuator fault-tolerant attitude control was reported. Two kinds of spacecraft actuator failures ...
This paper designs an active fault-tolerant control system for spacecraft attitude control in the pr...
In this paper, an improved robust model predictive controller (RMPC) is proposed based on model refe...
Actuator failures onboard spacecraft often lead to unsatisfied control performances or even the lose...
This article investigates the attitude stabilization problem of a rigid spacecraft with actuator sat...
In a control system, actuator failures may cause significant damaging effect on system performance o...
This paper studied the trajectory tracking control of a failure satellite that has actuator jumping ...