Purpose The purpose of this paper is to accomplish robust actuator fault isolation and
identification for microsatellite attitude control systems (ACSs) subject to a series of space …

For the satellite attitude control system with actuator and sensor fault, the paper proposes a
neural network based robust state and fault estimation method. Compared with the …

To improve the reliability of the attitude determination system with redundant gyroscopes,
this article proposes a gyroscope fault accommodation method using a bank of dedicated …

This paper focuses on the fault diagnosis method and the fault‐tolerant control method of the
aircraft with control surface damage. The fault diagnosis method is based on the set …

This paper proposes a novel self-healing control method for satellite attitude tracking based
on simultaneous fault estimation and control design. The proposed method integrates the …

The problem of PD-type Learning Observer (LO)-based fault reconstruction is addressed for
satellite attitude control systems in this paper. By introducing differential term of …

This paper presents a sensor fault diagnosis method for the satellite attitude determination
system based on analytical redundancy and wavelet transform. Specifically, we design a full …

This paper proposes a fault diagnosis approach for the satellite attitude determination
subsystem based on analytical redundancy and empirical mode decomposition (EMD) …

This paper proposes a fault-tolerant control method for discrete-time linear systems with
actuator fault. The proposed method is based on the fault hiding methodology. First, the …

The launch vehicle attitude control system is taken as the research object in this paper,
which is analyzed the function and composition of the system. A fault model of a certain type …